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Traveling Wave Tube Eigenmode Solver for Hot Slow Wave Structure Based on Particle-In-Cell Simulations

Tarek Mealy and Filippo Capolino Department of Electrical Engineering and Computer Science, University of California, Irvine, CA 92697, USA
[email protected] and [email protected]

I Introduction

Traveling wave tube (TWT) amplifiers are the devices of choice for several decades for radar and satellite communications applications when high power is required and also when reliability is important, like in satellite communications [1, 2]. TWTs are increasingly important to generate high power at millimeter wave and terahertz frequencies [3, 4, 5, 6, 7] where the current technology based on solid state devices struggles to generate even low power levels. An important component of the TWT is the slow wave structure (SWS), that is a guiding structure where the speed of the electromagnetic (EM) wave is reduced to match the speed of the beam electrons leading to energy transfer from the electron beam to the EM wave [8, 9]. An important mechanism for the energy transfer is the synchronization of the phase velocity vphv_{ph} of the EM wave in the SWS with the average speed of the electrons u0u_{0}. Furthermore, the EM wave needs to have a longitudinal electric field component EzE_{z} to interact with the electron beam to form electron bunches. Therefore the electron beam is modulated in terms of electron velocity and electron density forming a “space-charge wave” that is synchronized with the EM wave. The modes in the “hot” SWS are complex hybrid physical phenomena involving both the space-charge wave and EM field, i.e., each mode is made of these two components and may have a complex wavenumber.

The study of the “cold” eigenmodes in the SWS, i.e., the EM modes that exist without considering the interaction with the electron beam, is important to establish the onset of the synchronization condition between the electron beam’s space-charge wave and the EM wave in the SWS. Denoting with vphv_{ph} the phase velocity of the EM mode in the cold SWS and with u0u_{0} the average velocity of the electron beam, the initial synchronization condition is vphu0v_{ph}\approx u_{0}. There are various EM solvers in commercial software packages that can be used to find the dispersion diagram of the EM modes in the cold SWS. Some of the most famous commercial eigenmode solvers are provided by finite element method-based packages by Ansys HFSS and DS SIMULIA (previously known as CST Microwave Studio). Often, eigenmode solvers work under the approximation of a lossless SWS, i.e., the modes are found in a closed metallic waveguide with perfect electric conducting walls.

The interaction of an EM wave with the electron beam results in hybrid (EM+space-charge wave) modes whose phase velocity is different from the phase velocity of the cold EM eigenmode, hence the “hot” eigenmodes, i.e., the eigenmodes in interactive system, have a dispersion diagram that is different from the one of the cold EM modes, especially in the frequency region where vphu0v_{ph}\approx u_{0}. Although the study of the EM eigenmodes in a cold SWS is very important, the main operation of TWTs depends mainly on the eigenmodes of the hot SWS. Note that the modes of the interactive system have complex valued wavenumbers accounting for possible gain coming from the electron beam and losses in the metallic waveguide.

The modeling and design of TWTs are carried out by either theoretical models or simulations. For about the past seventy years, Pierce’s classical small signal theory has been used for the modeling and design of TWTs [10, 11]. Pierce describes the dispersion relation for hot SWS as cubic polynomial [10]. Other studies have been provided in the literature to theoretically model TWTs as in [12, 13, 14, 15, 16]. Although the theoretical models are considered as good tools for initial design of TWT, they are inaccurate and the actual performance of TWTs is assessed by performing accurate simulations.

Advances in 3D electromagnetic simulation software make it possible to accurately model and simulate complex electromagnetic structures accounting for the interaction with an electron beam. Most of the simulation and design work of TWTs is carried out using particle-in-cell (PIC) codes. A PIC solver is a self-consistent simulation method for particle tracking that calculates particles trajectories and EM fields in the time-domain [17, 18]. Some commercial computational software provides solvers based on PIC code that allows to accurately simulate driven-source problems of TWTs taking into account all physical aspects of the problem. Although PIC solvers are currently the most accurate tools to model TWTs, they require a lot of simulation time and computer memory size, especially for TWTs with large lengths, therefore, sometimes running multiple PIC simulations may not be the most practical way to start the optimization process. Several methods were proposed in literature as an intermediate step between simple qualitative theoretical models and time-consuming accurate PIC simulations. Some of thesemethods are based on merging data extracted from a 3D cold SWS electromagnetic simulator with those of a particle solver, assuming the SWS is modeled as 1D transmission line and the beam is modeled as pencil beam with infinitesimal cross-section area. These methods are used in the well known codes known as CHRISTINE [19, 20], TESLA [21]and MUSE [22]. Other methods based on merging results from 3D EM simulations and particle solver simulations are also proposed in [23, 24, 25, 26, 27].

In this paper, we present a method to model TWTs by finding the equivalent transfer matrix of a unit-cell based on accurate PIC simulations of a SWS with a relatively small number of unit-cells, which is not very time consuming. The advantage of extracting the SWS unit-cell transfer matrix is not only to infer the characteristics of the hybrid modes of the EM-beam interactive system (the main goal of this paper) but also to predict the behavior of longer structures without need to simulate it using PIC (left to future investigations). To date, no commercial software provides an eigenmode solver for hot SWSs taking into account the interaction with the electron beam and losses and the accurate geometry of the SWS.

The method shown in this paper is based on finding the unit-cell transfer matrix through the interpretation of data extracted from PIC simulation for relatively short SWSs. We show that the method is used to approximately calculates the complex wavenumbers of the hybrid modes supported in a hot SWSs. The method also provides the contribution of the EM wave and spatial charge wave to each specific hybrid mode associated to each of the complex modal wavenumbers. The proposed solver is based on accurate PIC simulations of finite length hot SWSs and takes account of the precise SWS geometry, materials’ EM properties, electron beam cross-section area, confinement magnetic field and space charge effect. The proposed solver is based on monitoring both the EM fields and electron beam dynamics in each unit cell and then find the best transfer matrix that describe how the hybrid EM field-electron beam propagates along the TWT as shown in Fig. 1. Some simplifying assumptions are made, like linearity of EM and space charge waves excited in the TWT, and the electron beam is assumed not to lose energy while it travels along the TWT as discussed in the next section. Notably, the method provides the dispersion diagram of complex valued wavenumbers versus frequency of all the hybrid modes supported in the interactive hot SWS.

II Theoretical framework

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Figure 1: (a) General setup used to determine the complex wavenumber versus frequency dispersion relation of hybrid modes in hot SWSs based on PIC simulations. In this figure we show a helix-based SWS, though the method is general and can be applied to several TWT structures. In (b) we show the associated circuit model where each unit cell of the hot SWS is modeled as a multi-port network circuit with equivalent voltages and currents representing EM waves (VnV_{n}, InI_{n}) and space-charge waves (VbnV_{bn}, IbnI_{bn}). In this figure, each unit cell has 4 ports, two for EM waves (with blue color) and two for space-charge waves (with red color). The method in this paper calculates the hybrid modes of the periodic SWS circuit made of periodically cascaded 4-port network unit cells. (c) Data flowchart used to extract the transfer matrix 𝐓u\mathbf{T}_{\mathit{u}} of a unit cell and then determine the hybrid eigenmodes of the hot SWS using the model in (b).

We demonstrate the performance of the proposed eigenmode to be periodically repeated solver by considering, as an illustrative example, the TWT made of a helix SWS with period dd consisting of NN unit-cells shown in Fig. 1. The input and output radio frequency (RF) signals of the structure are defined as Port 1 and Port 2. However, in the following both will be used as inputs in order to find the complex wavenumbers of the hybrid modes. It is important to point out that the following technique is general and can be applied to any kind of SWS, hence not only to helix-based SWSs. The PIC solver simulates the complex interaction between the guided EM wave and electron beam using a large number of charged particles and it follows their trajectories in self-consistent electromagnetic fields computed on a fixed mesh.

II-A Assumptions

The goal is to estimate the wavenumbers and composition of the hybrid modes of the interactive system made of EM field and the electron beam in a TWT amplifier as the one in Fig. 1. The method is based on finding the modes supported by the periodic distribution of equivalent networks shown in Fig. 1. Each unit cell is modeled using a transfer matrix which is calculated, as explained in this section, based on the results of accurate time domain PIC numerical simulations of the guided EM field interacting with the electron beam. The PIC method isbased oncharged particles motion equations and EM fields, discretized in space and time. Therefore, the EM field satisfies a discretized form of the time-domain Maxwell equations, and the PIC simulator accounts for the precise geometry and materials of the SWS and for the EM boundary conditions on the lateral walls of the periodic waveguide. Once time domain data are extracted from a PIC simulator, hybrid modes are found by imposing periodic boundary conditions along the TWT longitudinal direction z in the phasor domain using the periodic distribution of equivalent unit cell networks in Fig. 1, as discussed later on in this section. Therefore, the method estimates the complex wavenumbers of the hybrid EM-beam modes that exist in the infinitely-long sequence of equivalent unit cell networks in Fig. 1 by elaborating the data provided by the PIC method, simulating the EM field interacting with electrons in a realistic TWT of finite length. In Fig. 1 we show the data flowchart used to accomplish this task: the time domain data extracted from PIC simulations of relatively short SWSs are transformed into phasors and then used to find the unit-cell transfer matrix 𝐓u\mathbf{T}_{\mathit{u}} of which we find the eigenvalues and eigenvectors as described in this section.

In using and elaborating the data provided by the PIC solver, we make the following assumptions. Although a PIC solver calculates the speeds of discrete charged particles, we represent the longitudinal speed of all electron-beam charges as a one dimensional (1D) function ubtot(z,t)u_{b}^{tot}(z,t). This is achieved by averaging the speed of the charges at each z-cross section as described later on. Therefore, the electron-beam velocity and density are described by the functions ubtot(z,t)=u0+ub(z,t)u_{b}^{tot}(z,t)=u_{0}+u_{b}(z,t), and ρbtot(z,t)=ρ0+ρb(z,t)\rho_{b}^{tot}(z,t)=\rho_{0}+\rho_{b}(z,t), where u0u_{0} and ρ0\rho_{0} are the velocity and the density of the electrons in the unperturbed beam (i.e., the dc parts), and ub(z,t)u_{b}(z,t) and ρb(z,t)\rho_{b}(z,t) represent their modulation functions. In what follows, the structure is excited by monochromatic EM signals, hence we assume that the beam modulations ub(z,t)u_{b}(z,t) and ρb(z,t)\rho_{b}(z,t) are also monochromatic. We also assume that the ac modulation of the electron beam is small compared to the dc part, therefore the electron beam current is well approximated by the function ibtot(z,t)=I0+ib(z,t)i_{b}^{tot}(z,t)=-I_{0}+i_{b}(z,t), where I0I_{0} is the dc value and ib(z,t)i_{b}(z,t) is its time harmonic modulation, hence we neglect non linear effects. These assumptions are the same as in the Pierce model [10, 11], but the ac values are here calculated using averaging of results taken from time-domain PIC simulations as described later on in this section. All the calculations are based on the steady state regime in a TWT, therefore the time domain signals calculated by PIC are transformed into phasors thanks to the assumption that every ac quantity is sinusoidal.

We assume that the EM fields in the hot SWS of finite length are represented in phasor domain as superposition of modes of the infinitely-long hot SWS as

𝐄(x,y,z)=m𝐄modem(x,y,z),𝐇(x,y,z)=m𝐇modem(x,y,z),\begin{array}[]{c}\mathbf{E}(x,y,z)=\sum_{m}\mathbf{E}^{\mathrm{mode}m}(x,y,z),\\ \mathbf{H}(x,y,z)=\sum_{m}\mathbf{\mathbf{H}^{\mathrm{mode}\mathit{m}}}(x,y,z),\end{array} (1)

where 𝐄modem\mathbf{E}^{\mathrm{mode}m} and 𝐇modem\mathbf{H}^{\mathrm{mode}m} are the electric and magnetic fields of the mthm^{th} hybrid mode in the infinitely-long hot structure and they are assumed to be represented as a summation of Floquet spatial harmonics as

𝐄modem=ejkmodemzq𝐞modem(x,y)ej2πqz/d,𝐇modem=ejkmodemzq𝐡modem(x,y)ej2πqz/d,\begin{array}[]{c}\mathbf{E}^{\mathrm{mode}m}=e^{-jk^{\mathrm{mode}m}z}\sum_{q}\mathbf{e}^{\mathrm{mode}m}(x,y)e^{-j2\pi qz/d},\\ \mathbf{H}^{\mathrm{mode}m}=e^{-jk^{\mathrm{mode}m}z}\sum_{q}\mathbf{h}^{\mathrm{mode}m}(x,y)e^{-j2\pi qz/d},\end{array} (2)

indeed they are sampled with a spatial period d along the SWS. Our goal is to find the complex-valued wavenumbers kmodemk^{\mathrm{mode}m} and the eigenvectors of the hybrid beam-electromagnetic eigenmodes of the infinitely-long “hot” structure using PIC simulations of the finite-length structure. The discussion in the rest of the paper is based on linearity of the system with respect to the ac EM and space charge waves, and on the assumption that the electron beam does not lose energy along its travel along the TWT, therefore the dc electron beam velocity u0u_{0} is kept constant along the TWT. This assumption is important because we assume that the transfer matrix describing each periodic cell is the same along the whole SWS length.

The physical quantities that represent the EM modes in the interacting SWS are electric and magnetic fields 𝐄(x,y,z,t)\mathbf{E}(x,y,z,t) and 𝐇(x,y,z,t)\mathbf{H}(x,y,z,t) which are represented in terms of equivalent voltages and currents vn(t)v_{n}(t) and in(t)i_{n}(t) at discrete location of the periodic structure, where nn is the unit cell index number. In the rest of the paper we assume that only one cold EM mode is able to propagate in each direction of the cold SWS, hence only a single pair (vn,(v_{n},in)i_{n}) will be sufficient to describe the EM wave. Although these quantities cannot be uniquely defined in most kinds of waveguides, it is possible to define them and use them to model the space and temporal dynamics in a waveguide [28, 29, 30]. The space charge wave is represented by equivalent ac kinetic voltages and beam currents vbn(t)v_{bn}(t) and ibn(t)i_{bn}(t), respectively, using the averaging method in Fig. 2 as described next. We define a state vector that describes the EM and space-charge waves at locations z=zn=ndz=z_{n}=nd as

𝝍n(t)=[vn(t),in(t),vbn(t),ibn(t)]T.\mathbf{\boldsymbol{\psi}}_{n}(t)=[\begin{array}[]{cccc}v_{n}(t),&i_{n}(t),&v_{bn}(t),&i_{bn}(t)\end{array}]^{T}. (3)

In the following sections we explain how this state vector is calculated using PIC calculations at z=ndz=nd locations along the SWS. Since we assume that at steady state all the quantities involved in the state vector are monochromatic, we define a state vector in phasor-domain as

𝚿n=[Vn,In,Vbn,Ibn]T,\mathbf{\Psi}_{n}=[\begin{array}[]{cccc}V_{n},&I_{n},&V_{bn},&I_{bn}\end{array}]^{T}, (4)

assuming an implicit ejωte^{j\omega t} time dependence.

In the phasor domain we assume that the longitudinal propagation of the state vector satisfies the equation 𝚿n+1=𝐓u𝚿n\mathbf{\Psi}_{n+1}=\mathbf{T}_{\mathit{u}}\mathbf{\Psi}_{n}, where 𝐓u\mathbf{T}_{\mathit{u}} is the periodic unit cell transfer matrix, which is unknown and assumed invariant along the periodic cells of the SWS. As explained next, the first goal is to provide a method to estimate the transfer matrix 𝐓u\mathbf{T}_{\mathit{u}}. Then, we assume that each of the hybrid EM-charge wave mode in (1)-(2) is described by a state vector variation as 𝚿n=𝚿modemejkmnd\mathbf{\Psi}_{n}\mathbf{=\Psi}^{\mathrm{mode}m}e^{-jk_{m}nd}, where kmk_{m} is the complex wavenumber of such a mode. The goal of this paper is to find the complex wavenumbers kmk_{m} of all the hybrid modes in the hot SWS and to find the EM and beam modal weights in (4) for each of the hybrid modes. The goal is achieved by solving the eigenvalue problem

𝐓u𝚿modem=ejkmd𝚿modem,\mathbf{T}_{\mathit{u}}\mathbf{\Psi}^{\mathrm{mode}m}=e^{-jk_{m}d}\mathbf{\Psi}^{\mathrm{mode}m}, (5)

once the estimate of the transfer matrix 𝐓u\mathbf{T}_{\mathit{u}} has been calculated as described in the next two sections.

II-B Determination of the system state-vector

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Figure 2: Illustration of how the speed of the space-charge wave ubntotu_{bn}^{tot} is calculated at the entrance of the nthn^{th} unit-cell (at z=ndz=nd) using PIC simulation data. The space-charge wave speed at z=ndz=nd is calculated as the average of the speeds of the PIC-defined charges Su(t)S_{u}(t) that are in the proximity of z=zn=ndz=z_{n}=nd, i.e., in the small range defined as znΔz/2<zc(t)<zn+Δz/2z_{n}-\Delta_{z}/2<z_{c}(t)<z_{n}+\Delta_{z}/2, at time t. The subset of all the PIC-defined charges in this spatial interval at time t is called Sun(t)S_{un}(t) because are about to cross the section at z=znz=z_{n}. Since the set of Sun(t)S_{un}(t) is composed of many PIC-defined charges, we define their collection average ubntot=Sun¯u_{bn}^{tot}=\overline{S_{un}}, and the charge-wave equivalent kinetic voltage is vbntot=2ηubntot.v_{bn}^{tot}=\sqrt{2\eta u_{bn}^{tot}}.

For the particular illustrative example shown in Fig. 1, we define the voltage as the electric potential difference between helix loops and the host waveguide, as a function of the electric field via vn(t)=𝐞(t)𝐝nv_{n}(t)=\int\boldsymbol{\mathbf{e}}(t)\cdot\mathbf{d}\mathrm{\boldsymbol{\ell}}_{n}, where the index nn here represents the nthn^{th} unit-cell and 𝐝n\mathbf{d}\boldsymbol{\ell}_{n} is the incremental vector length along the path between the nthn^{th} helix loop and the host waveguide in the nthn^{th} unit-cell as shown in Fig. 3. An alternative way to define the voltage for the helix is presented in Appendix A. The current that equivalently represents the EM mode can be defined as the physical current flowing in the helix tape wire which is determined from the magnetic field using the integral in(t)=𝐡(t)𝐝𝐂ni_{n}(t)=\oint\mathbf{h}(t)\cdot\mathbf{d}\mathbf{C}_{n}, along the path CnC_{n} around a helix wire of the nthn^{th} unit-cell as shown in Fig. 1 (using the projection of this current along the z direction leads to the same result). It is important to point out that equivalent voltage and current representing the electric and magnetic fields can be similarly defined also for other SWSs (such as serpentine waveguides, overmoded waveguides, etc.) using the equivalent field representation described in [30, 29].

The PIC solver provides the speeds and locations of all the charged particles used to model the electron beam at any time tt. We define two dynamic sets that involve the speeds and coordinates zz of all the charges in PIC simulation at anytime instant tt as Su(t)={u1(t),u2(t),,uNq(t)}S_{u}(t)=\left\{u_{1}(t),u_{2}(t),...,u_{Nq}(t)\right\} and Sz(t)={z1(t),z2(t),,zNq(t)(t)}S_{z}(t)=\left\{z_{1}(t),z_{2}(t),...,z_{N_{q}(t)}(t)\right\}, respectively, where Nq(t)N_{q}(t) is the total number of charged particles used by the PIC simulator to model the electron beam at time instant tt. The space-charge wave modulating the electron beam is assumed to be represented using two physical quantities: the electrons speed which is expressed in term of the beam equivalent kinetic voltage vbtot(z,t)v_{b}^{tot}(z,t), and the space-charge wave current modulation ibtot(z,t)i_{b}^{tot}(z,t), as also described in Refs. [31, 32, 11]. The beam total equivalent kinetic voltage at the entrance of the nthn^{th} unit-cell is defined as vbntot(t)=2ηubntot(t),v_{bn}^{tot}(t)=\sqrt{2\eta u_{bn}^{tot}(t)}, where ubntot(t)=Sun(t)¯u_{bn}^{tot}(t)=\overline{S_{un}(t)} is the equivalent speed of the space-charge wave calculated as the average of the speeds of the set

Sun(t)={Su(t)|ndΔz2<Sz(t)<nd+Δz2},S_{un}(t)=\left\{\begin{array}[]{ccc}S_{u}(t)&|&nd-\dfrac{\Delta_{z}}{2}<S_{z}(t)<nd+\dfrac{\Delta_{z}}{2}\end{array}\right\}, (6)

that is defined by all the charged particles that are in vicinity of the entry of the nthn^{th} unit-cell (z=ndz=nd), and within the small spatial interval Δz\Delta_{z}, as illustrated in Fig. 2. The length of the spatial interval Δz\Delta_{z} is chosen to be very small, i.e, Δzλ0b/20\Delta_{z}\leq\lambda_{0b}/20, where λ0b=u0/f\lambda_{0b}=u_{0}/f, and u0u_{0} is the electron time-average speed and ff is the frequency modulating the space-charge wave. Although Δz\Delta_{z} is chosen to be small, it should be also large enough to contain a very large set of charged particles, as illustrated in Fig. 2. The charge-wave current at the nthn^{th} unit-cell (z=ndz=nd) is defined as ibntot(t)=ρbntot(t)ubntot(t)i_{bn}^{tot}(t)=-\rho_{bn}^{tot}(t)u_{bn}^{tot}(t), where ρbntot(t)\rho_{bn}^{tot}(t) is the electron beam charge density at the entry of the nthn^{th} unit-cell and is calculated as ρbntot(t)=qeNbn(t)/Δz\rho_{bn}^{tot}(t)=q_{e}N_{bn}(t)/\Delta_{z} where qeq_{e} is the charge value of each PIC-defined particle and Nbn(t)N_{bn}(t) is the number of such charged particles in the set Sun(t)S_{un}(t). The ac modulated parts are then calculated as vbn(t)=vbntot(t)V0v_{bn}(t)=v_{bn}^{tot}(t)-V_{0} and ibn(t)=ibntot(t)+I0i_{bn}(t)=i_{bn}^{tot}(t)+I_{0} which are used later on to construct the system’s state vector. As described below, when we calculate the phasor IbnI_{bn} associated to ibn(t)i_{bn}(t) we will retain only the frequency component at radian frequency 𝝎\mathbf{\boldsymbol{\omega}} and not the higher order harmonics.

It is important to point out that in this illustrative example we assume that the SWS supports one cold EM mode that can propagate in each direction and that the electron beam is represented by a single state that describes the average behavior of the speed and density of the charged particles distribution. Describing the EM-chanrge wave state using the four-dimensional state vector (3)constitutes a good approximation in many cases where the SWS supports only one EM mode (in each direction) and the electron beam is modulated in a homogeneous way, i.e., the beam modulation does not change with radial and azimuthal angular directions. However, a more accurate model of the hot SWS could be obtained by using an equivalent multi-transmission line model to describes all the EM modes in the SWS, and an equivalent multi “beam transmission line” (or multi stream beam) to describe the electron beam. Indeed, since we know that in reality the momentum and charge density description of the electron beam dynamics usually looks like a multi-valued function, it may be convenient to decompose the electron beam using various areas in transverse cross section leading to a multi “beam transmission line” with multiple kinetic voltages and space-charge wave currents. For the sake of simplicity, in this paper the electron beam dynamics is represented only with one “beam transmission line”, i.e., with a single (vb(t),ib(t)v_{b}(t),i_{b}(t)) pair.

The interaction between the space-charge wave and the EM wave yields three eigenmodes that travel in the beam direction in addition to a mode (mainly made of only EM field) propagating opposite to the beam direction, indeed the latter has very little interaction with the electron beam [11]. The three hybrid modes with positive phase velocity are composed of both EM fields and space-charge wave modulations, and form the “three-wave” model used in Refs. [33, 11]. Under the assumption of using a single tone excitation of an EM wave from Port 1 and/or Port 2, all four hybrid EM-charge wave modes in the interacting system can be excited: an excitation from Port 1 mainly excites the three interacting hybrid modes, whereas the excitation from Port 2 excites mainly the EM mode propagating in opposite direction of the beam. Reflections may occur at the left and right ends in a realistic finite-length SWS, so in reality all four modes may be present, depending on the EM reflection coefficients at the two ends.

At steady state, the state vector is represented in phasor-domain as in (4), assuming an implicit ejωte^{j\omega t} time dependence for all physical quantities. The phases of phasors are calculated with respect to a fixed time at steady state. The phasor-domain representation (4) of the state vector 𝝍n(t)\mathbf{\boldsymbol{\psi}}_{n}(t) is calculated as

𝚿n=1Tt=0t=T𝝍n(t+tref)ejωt𝑑t,\mathbf{\Psi}_{n}=\dfrac{1}{T}\int_{t=0}^{t=T}\mathbf{\boldsymbol{\psi}}_{n}(t+t_{ref})e^{-j\omega t}dt, (7)

where T=2π/ωT=2\pi/\omega and treft_{ref} is a time reference used to calculate the phasors and it should be greater than the steady state time, i.e., tref>tss.t_{ref}>t_{ss}. It is important to mention that only the fundamental component at frequency 𝝎\mathbf{\boldsymbol{\omega}} is maintained after the Fourier transform is carried out to build the state vector in phasor domain 𝚿n\mathbf{\Psi}_{n} in (4), hence all frequency harmonics in 𝝍n(t)\mathbf{\boldsymbol{\psi}}_{n}(t) are neglected in the following. Lower case letters are used for the time-domain representation whereas capital letters are used for the phasor-domain representation. In the phasor-domain, we model each unit cell of the interacting SWS as a 4-port network circuit with voltages and currents representing both the EM waves and the electron beam dynamics, as shown in Fig. 1. As described in the previous section, under the assumption of small signal modulation of the beam’s electron velocity and charge density, the 4-port networks modeling the EM-charge wave interaction in each unit-cell of the hot SWS are assumed identical. Therefore, one can define a 4×44\times 4 transfer matrix 𝐓u\mathbf{T}_{\mathit{u}} of the interaction unit-cell of a SWS using the relation between the input and output state vector at each unit-cell as

𝚿2=𝐓u𝚿1,(8.1)𝚿3=𝐓u𝚿2,(8.2)𝚿N+1=𝐓u𝚿N,(8.N)\begin{array}[]{c}\mathbf{\Psi}_{2}=\mathbf{T}_{\mathit{u}}\mathbf{\Psi}_{1},\ \ \ \ \ \ (\ref{eq:Tmatrix-StateVector}.1)\\ \mathbf{\Psi}_{3}=\mathbf{T}_{\mathit{u}}\mathbf{\Psi}_{2},\ \ \ \ \ \ (\ref{eq:Tmatrix-StateVector}.2)\\ \vdots\\ \mathbf{\Psi}_{N+1}=\mathbf{T}_{\mathit{u}}\mathbf{\Psi}_{N},\ \ \ \ \ \ (\ref{eq:Tmatrix-StateVector}.N)\end{array} (8)

where 𝚿n+1\mathbf{\Psi}_{n+1} and 𝚿n\mathbf{\Psi}_{n} are the input and output state vectors of the nthn^{th} unit-cell, respectively, where n = 1, 2,.. N. The state vectors 𝚿n\mathbf{\Psi}_{n} are calculated from ψn\mathbf{\psi}_{n} using PIC simulations; then an estimate of the transfer matrix 𝐓u\mathbf{T}_{\mathit{u}} is inferred by the method described in the following section.

II-C Finding the transfer matrix of a unit cell of the interactive system

II-C1 Approximate best fit solution

The relations in (8) represent 4N4N linear equations in 1616 unknowns which are the elements of the transfer matrix 𝐓u\mathbf{T}_{u}. The system in (9) is mathematically referred to as overdetermined because the number of linear equations (4N4N equations) is greater than the number of unknowns (16 unknowns). We rewrite (8) by clustering all the given equations in matrix form as

[𝐖2]4×N=[𝐓u]4×4[𝐖1]4×N\left[\mathbf{W}_{2}\right]_{4\times N}=\left[\mathbf{T}_{\mathit{u}}\right]_{4\times 4}\left[\mathbf{W}_{1}\right]_{4\times N} (9)

where

𝐖1=[𝚿1,𝚿2,𝚿N]\mathbf{W}_{1}=\left[\begin{array}[]{cccc}\mathbf{\Psi}_{1},&\mathbf{\Psi}_{2},&\ldots&\mathbf{\Psi}_{N}\end{array}\right] (10)

is a 4×N4\times N matrix and its columns are the state vectors at input of each unit-cell, and

𝐖2=[𝚿2,𝚿3,𝚿N+1]\mathbf{W}_{2}=\left[\begin{array}[]{cccc}\mathbf{\Psi}_{2},&\mathbf{\Psi}_{3},&\ldots&\mathbf{\Psi}_{N+1}\end{array}\right] (11)

is an analogous 4×N4\times N matrix but with a shifted set of the state vectors, i.e., its columns are the state vectors at the output of each unit-cell. Our first goal is to find the 16 elements of the transfer matrix 𝐓u\mathbf{T}_{\mathit{u}}.

An approximate solution that best satisfies all the given equations in Eq. (8), i.e., minimizes the sums of the squared residuals, n𝚿n+1𝐓u𝚿n\sum_{n}\left|\left|\mathbf{\Psi}_{n+1}-\mathbf{T}_{\mathit{u}}\mathbf{\Psi}_{n}\right|\right| is determined similarly as in [34, 35, 36] and is given by

𝐓u,𝑏𝑒𝑠𝑡=([𝐖2]4×N[𝐖1]4×NT)([𝐖1]4×N[𝐖1]4×NT)1.\mathbf{T}_{\mathit{u,best}}=\left(\left[\mathbf{W}_{2}\right]_{4\times N}\left[\mathbf{W}_{1}\right]_{4\times N}^{T}\right)\left(\left[\mathbf{W}_{1}\right]_{4\times N}\left[\mathbf{W}_{1}\right]_{4\times N}^{T}\right)^{-1}. (12)

It is important to point out that all the four modes of the interactive EM-charge wave system should be excited to be able to have four independent columns in the construction of the matrices 𝐖1\mathbf{W}_{1} and 𝐖2\mathbf{W}_{2} since we need apply the inverse operation in (12). This occurs when there is sufficient amount of power incident on Port 1 and Port 2.

II-C2 Distinct determined solutions

The transfer matrix 𝐓u\mathbf{T}_{\mathit{u}} can also be determined directly by taking any four equations of Eq.(8), assume we choose Eq. (8.q)q), Eq. (8.i)i), Eq. (8.j)j) and Eq. (8.k)k), and therefore yields

𝐓u,𝑞𝑖𝑗𝑘=[𝐰2,qijk]4×4[𝐰1,qijk]4×41,\mathbf{T}_{\mathit{u,qijk}}=\left[\mathbf{w}_{2,qijk}\right]_{4\times 4}\left[\mathbf{w}_{1,qijk}\right]_{4\times 4}^{-1}, (13)

where

𝐰1,qijk=[𝚿q,𝚿i,𝚿j,𝚿k]\mathbf{w}_{1,qijk}=\left[\begin{array}[]{cccc}\mathbf{\Psi}_{q},&\mathbf{\Psi}_{i},&\mathbf{\Psi}_{j},&\mathbf{\Psi}_{k}\end{array}\right] (14)

and

𝐰2,qijk=[𝚿q+1,𝚿i+1,𝚿j+1,𝚿k+1].\mathbf{w}_{2,qijk}=\left[\begin{array}[]{cccc}\mathbf{\Psi}_{q+1},&\mathbf{\Psi}_{i+1},&\mathbf{\Psi}_{j+1},&\mathbf{\Psi}_{k+1}\end{array}\right]. (15)

Assuming the SWS has NN unit cells, there will be C4NC_{4}^{N} possible solutions for 𝐓u,qijk\mathbf{T}_{u,qijk} , where C4N=N!/((N4)!4!)C_{4}^{N}=N!/((N-4)!4!) is the number of the combinations to choose q,i,jq,i,j and kk out of NN choices. Under the assumption that the transfer matrices of each unit-cell are identical, the sets of four eigenvalues resulting from the C4NC_{4}^{N} solutions of 𝐓u,qijk\mathbf{T}_{u,qijk} should be identical too. However, the electron beam non-linearity and other factors may cause small discrepancy in the eigenvalues resulting from the various eigenmode solutions of 𝐓u,qijk\mathbf{T}_{u,qijk} , as shown in the next section.

It is important to point out that some combinations may result in a underdetermined system where the rank of 𝐰1,qijk\mathbf{w}_{1,qijk} could be less than 4, i.e., 𝐰1,qijk\mathbf{w}_{1,qijk} could be singular. For example, when selecting unit cells toward the right end of the TWT (e.g., q=N3,i=N2,j=N1q=N-3,i=N-2,j=N-1 and k=Nk=N), the state vectors forming 𝐰1.qijk\mathbf{w}_{1.qijk} are dominated by only one mode that has exponential growing in zz direction, and therefore the matrix 𝐰1,qijk\mathbf{w}_{1,qijk} tends to be singular. Therefore, one can neglect combinations that are close to be singular by checking the determinant of 𝐰1,qijk\mathbf{w}_{1,qijk} for each combination. Following this method, multiple transfer matrices are found that lead to multiple wavenumbers that are clustered around four complex values.

II-D Finding the hybrid eigenmodes of the interactive system

Once the transfer matrix is estimated (either using the best-approximate solution 𝐓u,𝑏𝑒𝑠𝑡\mathbf{T}_{\mathit{u,best}} of the overdetermined system or determined solutions 𝐓u,qijk\mathbf{T}_{u,qijk}), the hybrid eigenmodes are determined by assuming a state vector has the form of 𝚿nejknd\mathbf{\Psi_{\mathrm{\mathit{n}}}}\propto e^{-jknd}, where kk is the complex Bloch wavenumber that has to be determined and dd is the SWS period. Inserting the assumed sate vector z-dependency in (8) yields the eigenvalue problem in (5). Note that eigenvalues ejkde^{-jkd} and eigenvectors 𝚿n\mathbf{\Psi}_{n} of the eigenvalue problem in (5) depend only on the transfer matrix 𝐓u\mathbf{T}_{u}. The four eigenvalues,

ejkd=eig(𝐓u),e^{-jkd}=\mathrm{eig}(\mathbf{T}_{\mathit{u}}), (16)

of the transfer matrix 𝐓u\mathbf{T}_{\mathit{u}} lead to four Floquet-Bloch modes kmk_{m}, where m=1,2,3,4m=1,2,3,4, with harmonics km+2πq/dk_{m}+2\pi q/d, where qq is an integer that defines the Floquet-Bloch harmonic index as in (2). Some examples are provided in the next sections. Note that (5) provides also the eigenvectors 𝚿modem\mathbf{\Psi}^{\mathrm{mode}m} and important information can be extracted from them. Each mthm^{th} eigenvector possesses the information of the respective weights of the EM field (V,IV,I) and space-charge wave (Vb,IbV_{b},I_{b}) in making that particular hybrid eigenmode solution. Furthermore, including the case when more EM modes are used in the SWS interaction zone or when two hybrid modes concur in the synchronization, an analysis of the eigenvectors can also show possible eigenvector degeneracy conditions. For example, in [37, 38, 39], two hybrid modes are fully degenerate in wavenumbers and eigenvectors forming what was called a “degenerate synchronization” (degeneracy between two hot modes). Other important degeneracy conditions are those studied in [40], where three or four fully degenerate EM modes in the cold SWS are used in the synchronization with the electron beam, a condition refer to as “multimode synchronization” (degeneracy among cold EM modes).

In a finite length TWT, the total EM field (represented by VntotV_{n}^{\mathrm{tot}}, IntotI_{n}^{\mathrm{tot}} ) and space-charge wave (represented by VbntotV_{bn}^{\mathrm{tot}}, IbntotI_{bn}^{\mathrm{tot}}) resulting from their interaction, calculated at each nthn^{th} location, are represented in terms of the four eigenmodes,

𝚿ntot=m=14am𝚿modemejkmnd\mathbf{\Psi}_{n}^{\mathrm{tot}}=\sum_{m=1}^{4}a_{m}\mathbf{\Psi}^{\mathrm{mode}m}e^{-jk_{m}nd} (17)

where ama_{m} is the weight of the mthm^{th} mode, which depends on the mode excitation and boundary conditions, and 𝚿modem\mathbf{\Psi}^{\mathrm{mode}m} is the interactive system eigenvectors obtained from (5). Each Floquet-Bloch mode in the periodic hot SWS is represented as 𝚿modemejkmnd\mathbf{\Psi}^{\mathrm{mode}m}e^{-jk_{m}nd}.

In this paper we show how to determine the eigenvector 𝚿modem\mathbf{\Psi}^{\mathrm{mode}m} and wavenumber kmk_{m} of each of the four hybrid eigenmodes (m=1,2,3,4m=1,2,3,4), using two illustrative examples: a centimeter wave (i.e., “microwave”) and a millimeter wave TWT amplifier.

III Application to a helix-based TWT amplifier

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Figure 3: (a) Geometry of the SWS of a TWT amplifier made of a circular metallic waveguide and a copper helix with three dielectric supports. RF input and output are through the coaxial Ports 1 and 2. (b) Circuit model and numbering scheme used to construct the state vectors that are used to determine the interactive system transfer matrix. Each unit cell has four ports with equivalent voltages and currents: (VnV_{n}, InI_{n}) for the two EM ports and (VbnV_{bn}, IbnI_{bn}) for the two electron beam ports, therefore each unit cell is described by a 4×44\times 4 transfer matrix 𝐓u\mathbf{T}_{u}.

We demonstrate how the technique described in the previous section is applied considering an illustrative example made of a C-Band TWT amplifier described in [41] and shown in Fig. 3. Such TWT amplifier operates at 4 GHz and uses a solid linear electron beam with radius of 0.63 mm, with dc kinetic voltage of 3 kV and dc current of 75 mA. The axial dc magnetic field used to confine the electron beam is 0.6 T. The TWT uses a copper helix tape with inner radius of 1.26 mm and period of d=d=0.76 mm, and the metallic tape has 0.1750.175 mm thickness and 0.3250.325 mm width. The metallic circular waveguide has radius of 33 mm and the three supports that physically hold the helix are made of Anisotropic Pyrolytic Boron Nitride (APBN) with relative dielectric constant of 5.12 and and with width of 0.70.7mm. The numerical simulation consists of 15 periods of the structure. We show the numbering scheme used to define the voltages and currents representing the EM wave and the space-charge wave at the begin and end of each unit-cell in Fig. 3. While the whole structure is considered in PIC simulations, when we apply the proposed method we do not consider the first and the last state vectors (i.e., at the beginning and end of of the first and last unit cells) because the begin and the end of the SWS are close to the coaxial waveguide input and output ports, and higher order modes due to the transformation of the TEM wave in the coaxial waveguide into the SWS modes would influence the calculation of the unit-cell transfer matrix.

First, we study the system eigenmodes at single frequency by exciting Port 1 and Port 2 with 10 Watt and 5 Watt, receptively, at 4 GHz. Note that indeed, even if the actual TWT operation involves feeding from one side only, the scheme explained in the above section may need a SWS feed from both the left and right ports to be sure we excite all the modes. It is important to mention that changing the power levels at Port 1 and Port 2 shall not significantly affect the resulting eigenmode solution as long as the power levels are not too high to involve non-linear regimes. The total number of charged particles used to model the electron beam in the PIC simulation is about 10610^{6} whereas the whole space in the SWS structure is modeled using 8×1058\times 10^{5} mesh cells. Once steady state is reached, the time-domain state vector 𝝍n(t)\mathbf{\mathbf{\boldsymbol{\psi}}}_{n}(t) is monitored at each nthn^{th} unit-cell. Figure 4 shows the four components (3) of the state vector at the 3rd3^{rd}, 8th8^{th} and 13th13^{th} unit cells in the time interval between 79T79T and 80T80T, where T=0.25T=0.25 ns is the time period at 4 GHz. The phasor-domain representation (4) of the state vector 𝚿n\mathbf{\Psi}_{n} is calculated using (7) with tref=79T=19.75t_{ref}=79T=19.75 ns.

The four wavenumbers of the eigenmodes of the interacting SWS system are shown in Fig. 5 based on results from Eq. (9) leading to the four red crosses, and from Eq. (13) leading to the various blue dots. The scattered blue dots represent 75 sets of four complex wavenumbers associated with 75 sets of transfer matrices obtained from Eq. (13) using 75 combinations of q,i,jq,i,j and kk to give the highest 75 determinants of the matrix 𝐰1,qijk\mathbf{w}_{1,qijk} out of the all 330 combinations. It is important to mention that the solutions associated with the rest 255 combinations q,i,jq,i,j and kk were ignored because they result in almost singular matrices 𝐰1,qijk\boldsymbol{\mathrm{w}}_{1,qijk} and 𝐰2,qijk\boldsymbol{\mathrm{w}}_{2,qijk}.

The results in Fig. 5 show a good agreement between the red crosses that represent the four wavenumbers obtained from the eigenvalues of 𝐓u,best\mathbf{T}_{u,best} where 𝐓u,best\mathbf{T}_{u,best} is the best-approximate solution of the overdetermined system in (9) and the blue dots that represent the eigenmodes of various estimates of 𝐓u,qijk\mathbf{T}_{u,qijk} obtained from solutions of (13). It is important to point out that the small deviations between the complex wavenumbers obtained from different solutions is due to non-idealities resulting in having non-identical unit-cells along the structure. This may happen due to the electron beam non-linearity and the change of the beam kinetic voltage along the TWT, in addition to the errors due to finite mesh and finite number of charged particles used to model the TWT dynamics. The resulting eigenmodes are qualitatively in good agreement with the expected description using the theoretical transmission line-based Pierce model [11] that basically says that there exist three wavenumbers with positive real part, and one of them has positive imaginary part which describes the amplification of the EM wave along the SWS.

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Figure 4: Time-domain state vector 𝝍n(t)\mathbf{\boldsymbol{\psi}}_{n}(t) monitored at different n=3,8,13n=3,8,13 locations of TWT at steady state: at the entrance of the (a) 3rd3^{rd}, (b) 8th8^{th} and (c) 13th13^{th} unit-cell. The four plotted quantities are provided by a full-wave simulation based on the particle-in-cell (PIC) method. The phasor-domain representations of the state vectors 𝚿n\mathbf{\Psi}_{n} (3n143\leq n\leq 14 ) to be used in the proposed method to find the modal dispersion are calculated from the time domain signals (vn,in)(v_{n},i_{n}) and (vbn,ibn)(v_{bn},i_{bn}).
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Figure 5: Determination of the four complex wavenumbers kmk_{m} of the four eigenmodes (m=1,2,3,4m=1,2,3,4) in the interactive (hot) electron beam-EM mode in the helix-based SWS at f=4f=4 GHz, when using a beam voltage and current of 33 kV and 7575 mA, respectively. The wavenumbers are normalized to space-charge wave wavenumber β0=ω/u0\beta_{0}=\omega/u_{0} of the beam alone, i.e., when it does not interact with the EM wave. The red crosses represent the four wavenumbers obtained from the eigenvalues of the transfer matrix 𝐓u,best\mathbf{T}_{u,best}, where 𝐓u,best\mathbf{T}_{u,best} is the best-approximate solution of the overdetermined system in (8). The blue dots represent different sets of four wavenumbers obtained from the eigenmvalues of different sets of transfer matrices 𝐓u,qijk\mathbf{T}_{u,qijk}, where 𝐓u,qijk\mathbf{T}_{u,qijk} are the solutions obtained from (13) using different combinations of indices q,i,jq,i,j and kk.

The wavenumber-frequency dispersion describing the eigenmodes in the hot SWS is determined by running multiple PIC simulations at different frequencies and then determining the transfer matrix of the unit-cell at each frequency using Eq. (9), i.e., the result shown by the red crosses. In other words we repeat the red-cross results shown in Fig. 5 at various frequencies. The dispersion diagram of the four modes in the hot EM-electron beam system is shown in Fig. 6 (solid lines) using 42 frequency points (42 PIC simulations). The dashed red and blue lines represent the space-charge wave (i.e., the beam line) and EM modes when they are uncoupled (i.e., in the “cold” case). The dispersion of the EM mode in the cold SWS (dashed black) is found by the finite element method-based eigenmode solver implemented in CST Studio Suite by numerically simulating only one unit-cell of the cold helix SWS.

The black solid line in Fig. 6 is the hybrid mode propagating with Re(k)\mathrm{Re}(k)<0, i.e., in opposite direction of the beam flow and basically no beam-EM interaction occurs, and it is made mainly of EM field as also explained later on in Fig. 7. Indeed, as compared to the cold EM modes, the solid-black line of the hot SWS simulation is superposed to the dispersion line of the cold EM mode propagating in the negative zz-direction.

The three eigenmodes with wavenumbers with positive real part (solid red, green, blue lines) are the eigenmodes affected by the interaction between the electron beam’s space-charge wave and the EM wave propagating in the same direction. The solid-red curve in the dispersion relation has Im(k)\mathrm{Im}(k)>0 and represents the growing eigenmode that causes the amplification of the EM wave. The imaginary part of the growing mode starts to decreases with increasing frequency because the difference between the speed of the space-charge wave and that of the EM wave in the SWS (when we consider them uncoupled) increases. It is important to mention that a single PIC simulation could also be investigated to find the dispersion relation when using a moderately wide-band gaussian pulse at the input ports, however it would require excessive post processing to be able to decompose each tone behavior and it does not fully account for steady state regime resulting from the interaction with the electron beam that would otherwise includes also non-linear effects.

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Figure 6: Hot dispersion diagram for the four complex wavenumbers versus frequency for the beam-EM wave interactive system made of the hot helix-based SWS working at C-Band, using an electron beam with 33 kV and 7575 mA. Dashed lines describe the cold case: the dashed red line represents the wavenumber of the space-charge wave β0=ω/u0\beta_{0}=\omega/u_{0} whereas the black dashed line represents the wavenumber of cold SWS; i.e., assuming no interaction. There are three complex (interactive) modes with positive-real part of the wavenumber, in agreement with Pierce theory [11].

The hybrid modes describing the EM-charge wave interaction are further understood by looking also at their eigenvectors, besides their wavenumbers. Eigenvectors satisfy Eq. (5) and are the same used in the aforementioned discussed method to find the transfer matrix. The eigenvectors components in (4) describe the relative weight of the EM wave (VV, II) versus the space-charge wave (Vb(V_{b}, Ib)I_{b}), for each of the four modes 𝚿modem\mathbf{\Psi}^{\mathrm{mode}m}, with m = 1,2,3,4. The relative strength of the EM wave and space-charge wave in each eigenmode is determined in Fig. 7 by calculating the ratio between between the ac electron beam current and the EM mode equivalent transmission line current. The ratio |Ib/I||I_{b}/I| for each of the four eigenmodes is shown using colors consistent with those in Fig. . The figure verifies that the eigenmode with EM wave propagating with Re(k)\mathrm{Re}(k)<0 (solid-black line), in the direction opposite to the electron beam flow does not interact with the electron beam since the beam ac current component associated to this mode is vanishing. The growing eigenmode (Im(k)\mathrm{Im}(k)>0), red line, is the one responsible of EM amplification and it shows a good EM-charge wave interaction from 3.6 GHz to 4.2 GHz which is in agreement with the bandwidth specification of the amplifier given in [41]. Indeed, the operation of TWT as an amplifier depends on having a spatially growing mode (along the SWS) and the only mechanism to have a growing mode is via the coupling to the electron beam that gives back power to the EM wave after electron bunching is formed. This plot indeed shows that the red mode is the result of synchronization and generate a very strong electron beam.

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Figure 7: Ratio of the magnitudes of the phasors representing the electron beam ac current and EM-wave equivalent-transmission line current versus frequency when the electron beam has adc kinetic voltage of 33 kV and dc current of 7575 mA. The growing mode with Im(k)\mathrm{Im}(k)>0 (solid red) is composed of a strong charge-wave component. The hybrid mode with Re(k)\mathrm{Re}(k)<0 (solid-black) is mainly made of EM field, as expected.

A synchronization study is performed by observing the modes’ complex wavenumber when sweeping the beam dc voltage. In Fig. 8 we show the wavenumbers for the three hot eigenmodes with positive real part (red, green, and blue curves) when changing the beam dc kinetic voltage V0V_{0} while the dc beam current is maintained at 75 mA, at a constant frequency of 4 GHz. Solid lines represent the three eigenmodes in the interactive (i.e., hot) SWS, whereas the dashed lines represent the beam line β0=ω/u0\beta_{0}=\omega/u_{0} (red dashed) and the cold EM mode with positive wavenumber (i.e., in the cold SWS). Since the frequency is fixed the cold EM mode has a fixed wavenumber βph=\beta_{ph}=999.8 m1\mathrm{m}^{-1} and it is described by the vertical black-dashed line. The phase velocity of the EM mode in the cold SWS is vph=ω/βph=0.084cv_{ph}=\omega/\beta_{ph}=0.084c since ω=2π(4×109)\omega=2\pi(4\times 10^{9}) rad/s, where c=3×108c=3\times 10^{8}m/s is the speed of waves in free space. Synchronization occurs approximately in the region where the two dashed lines, beam line and EM-wave line, have the same wavenumber, i.e., the same phase velocity, which happens just above 1.8 kV. The TWT amplification factor, mainly represented by the positive imaginary part of the red eigenmode, shows a peaking around synchronization point of V0=V_{0}=1.8 kV which is corresponding to a beam speed u0=2ηV0=0.084cu_{0}=\sqrt{2\eta V_{0}}=0.084c, where η=e/m\eta=e/m is the charge to mass ratio of the electron.

At lower or much higher dc voltage with respect to the synchronization point would make the beam-EM interaction is weak. This is also understood by noting that the gain starts to decay away from the interaction voltage region and the hot modes (resulting from the interaction) tend to overlap with the cold modes (without interaction) away from such region. In particular at low frequency the solid green curve tends to overlap with the cold EM mode, whereas at high frequency the solid blue line tends to overlap with the cold EM mode. The two solid red and blue curves at low dc voltage tend to overlap with the beam curve (red dashed), whereas the two solid red and green curves at high voltage tend to overlap with the beam line (red dashed): therefore these hot modes tend to overlap with the beam line (non-interactive beam) at high and low voltage despite some shifts which may be due to space charge effects. Near the synchronization point, the splitting of the solid green and blue curve (versus the red curve that does not split) represent the strong interaction between the electron beam and the EM field.

In Fig. 8 we show the complex plane mapping of the wavenumbers for the three hot eigenmodes with Re(k)>0\mathrm{Re}(k)>0, shown in Fig. 8, varying the electron beam dc voltage V0V_{0} (i.e., the speed of the electrons u0u_{0}). The black dots represent the interactive modes wavenumbers when the beam dc voltage is V0=1.8V_{0}=1.8 kV which results in an electron beam with average speed very close to the EM mode in the cold SWS, i.e., close to the synchronization point u0vphu_{0}\approx v_{ph}. The complex wavenumber location of the three interactive modes shown in Fig. 8 is in agreement with the three-wave theory of the Pierce model [33, 11] around the synchronization point. When u0vphu_{0}\approx v_{ph}, there are three modes with Re(k)\mathrm{Re}(k)>0: two of them are waves that are slower than the electron beam average speed u0vphu_{0}\approx v_{ph}, and among these two, one wave is growing in the beam direction while the other one is decaying. The third mode is basically an unattenuated wave that travels faster than the beam-average speed u0vphu_{0}\approx v_{ph}.

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Figure 8: Eigenmodes complex wavenumbers for the hot helix-based SWS at frequency f=4f=4 GHz versus beam dc kinetic voltage V0V_{0} (i.e., versus electron velocity u0=2ηV0u_{0}=\sqrt{2\eta V_{0}}) at constant dc current of 7575 mA. Only the three (interactive) modes with positive-real part of the wavenumber are shown. The amplifying mode is represented by the red-solid curve that has Im(k)\mathrm{Im}(k)>0. (a) kV0k-V_{0} dispersion. The vertical dashed black line represents the wavenumber of the EM wave in the cold SWS, whereas the dashed red curve represents the beam space-charge wave u0=ω/β0u_{0}=\omega/\beta_{0} without interaction with the EM wave. (b) Corresponding complex plane plot for the wavenumbers in (a), where the black dots represent the three complex modes at the synchronization point where u0vphu_{0}\approx v_{ph} at V0=1.8V_{0}=1.8 kV. The wavenumbers of modes in the hot SWS are in good agreement with the Pierce model around the synchronization point [33, 11].

The power flow for each mode of the hot (i.e. interactive) SWS is written in the form of Pm(z)=P0,me2Im(km)zP_{m}(z)=P_{0,m}e^{2\mathrm{Im}(k_{m})z} [42], where P0,mP_{0,m} is the initial amount of power carried by the same mode at z=0z=0. We define the power gain resulting from the interaction between the EM and space-charge wave for as Gp,m(z)=Pm(z)/P0,m=e2Im(km)z.G_{p,m}(z)=P_{m}(z)/P_{0,m}=e^{2\mathrm{Im}(k_{m})z}. Thus gain growth rate for each mode is 20log(e)Im(km)20\log(e)\mathrm{Im}(k_{m}) dB/m. In Figure 9 we show the gain growth rate for the three interactive modes (those with Re(km)>0\mathrm{Re}(k_{m})>0) versus electron-beam charges average speed u0=2ηV0u_{0}=\sqrt{2\eta V_{0}} (normalized by the cold SWS phase velocity vph=ω/βphv_{ph}=\omega/\beta_{ph} , where βph\beta_{ph} is the wavenumber of the EM mode in the cold SWS). The figure shows that there is an optimal point for the interaction (where u0/vph1.18u_{0}/v_{ph}\approx 1.18) which is very close to synchronization point where the power transfer from the kinetic energy of the electron beam into RF power in the SWS is maximum, as discussed in [43, 10]. The figure also show that the largest power transfer, from the kinetic energy of the electron beam into RF power, occurs when the average speed of electron beam charges is roughly above the speed of the cold EM wave in the SWS.

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Figure 9: Gain growth rate defined for the three interactive modes in the hot helix-based SWS versus the electron beam average speed u0u_{0} normalized to the cold SWS phase velocity. We change the electron beam speed u0u_{0} through varying the beam dc kinetic voltage V0V_{0} (u0=2ηV0u_{0}=\sqrt{2\eta V_{0}}). As in Fig. 8, the beam dc current is 7575 mA and f=4f=4 GHz, hence the cold EM mode phase velocity is constant vph=0.084cv_{ph}=0.084c . The amplifying mode is represented by the red-solid curve. The point where the gain growth rate is maximum is close to the synchronization point when u01.2vph.u_{0}\approx 1.2v_{ph}.

In Appendix A we show the effect of changing the voltage definition and the SWS length on the eigenmode calculations for the same helix SWS considered in this section. There, we define the voltages representing the EM waves as the potential differences between each two successive helix loops. Results are qualitatively in agreement with what described here, and only small quantitative differences are observed.

IV Application to serpentine-based TWT amplifier

We demonstrate the utility of the proposed eigenmode solver method to find the eigenmodes in the hot serpentine SWS operating at a millimeter wave band. The interaction with the electron beam is periodic and not uniform as for the case of the helix SWS. Serpentine SWSs have recently gained a lot of interest due to the growing importance of millimeter wave and terahertz frequencies in modern applications and also due to the advancement of fabrication technologies such as LIGA (LIthographie, Galvanoformung, Abformung). As an illustrative example, we use the same geometry of serpentine SWS discussed in [44, 45], as shown in 10. The serpentine waveguide is made of copper and has rectangular cross-section of dimensions a=1.9a=1.9 mm and b=0.325b=0.325 mm, bending radius of 0.3250.325 mm (radius at half way between inner and outer radii), straight section length of 0.6 mm, beam tunneling radius of 0.1750.175 mm. The TWT comprises 13 unit-cells . An electron beam with dc voltage V0=20V_{0}=20 kV is used such that the synchronization occurs with a forward EM wave leading to amplification. In Fig 10 we show the beam line β0=ω/u0\beta_{0}=\omega/u_{0} (red line) where u0=2ηV0=0.28cu_{0}=\sqrt{2\eta V_{0}}=0.28c, and the dispersion diagram of EM modes in the cold SWS (black line). Synchronization, vphu0v_{ph}\approx u_{0}, between the electron beam and the forward EM wave occurs at frequencies centered at f=88f=88 GHz.

Figure 10 shows the setup used for PIC simulations. We consider the electron beam to have a radius of 0.13 mm, a dc current of 0.10.1 A and an axial confinement dc magnetic field of 0.6 T. Our goals is to obtaining the dispersion of the hot serpentine SWS, i.e., the complex wavenumber of the hybrid modes that account for the interaction between the electron beam and the EM wave. In our method we excite the SWS from Port 1 with 10 Watts and from Port 2 with 5 Watts. An amplifier has the input at one port and the output at the other one, but here we want to excite the supported eigenmodes sufficiently to be observed in the calculations. The serpentine supports the TE10\mathrm{TE_{10}} mode which is the only one propagating in the rectangular waveguide. Since the serpentine waveguide does not support a TEM mode, voltage and current cannot be uniquely defined. We use the equivalent representation in [28, 30, 29] that models the waveguide as a transmission line with equivalent voltage and current. Following the derivations in [28, 30, 29] for the TE10\mathrm{TE_{10}} mode in a rectangular waveguide, the transverse fields are written as

Ey(x,y,z)=V(z)2absin(πxa),Hx(x,y,z)=I(z)2absin(πxa).\begin{array}[]{c}E_{y}(x,y,z)=V(z)\sqrt{\dfrac{2}{ab}}\sin\left(\dfrac{\pi x}{a}\right),\\ H_{x}(x,y,z)=I(z)\sqrt{\dfrac{2}{ab}}\sin\left(\dfrac{\pi x}{a}\right).\end{array} (18)

Using (18), the discrete voltages and the currents that represent the EM state at different rectangular cross-sections of the serpentine waveguide are found as

Vn=ab2Eyn,In=ab2Hxn,\begin{array}[]{c}V_{n}=\sqrt{\dfrac{ab}{2}}E_{yn},\\ I_{n}=\sqrt{\dfrac{ab}{2}}H_{xn},\end{array} (19)

where EynE_{yn} and HxnH_{xn} are the traverse electric and magnetic fields calculated at the center of the rectangular (x=a/2x=a/2 and y=b/2y=b/2) waveguide cross section as shown in the inset in Fig. 10 and they are calculated at the unit cells boundaries shown in Fig. 10.

We start by studying the eigenmode wavenumbers in the interacting SWS system at constant frequency f=88f=88 GHz, which is very close to the synchronization point where u0=vphu_{0}=v_{ph}. The four complex wavenumbers of the hybrid modes are shown in Fig. 11 based on results from Eq. (9) leading to the four red crosses, and from Eq. (13) leading to various blue dots. The scattered blue dots represent 37 sets of four complex wavenumbers associated the largest 37 determinants of the matrix 𝐰1,qijk\mathbf{w}_{1,qijk} out of the all 126 combinations. The blue dots cluster around the four red crosses, as expected. It is important to mention that we ignored the state vectors of the first and the last two unit cells to generate our results because they may involve high order modes that affect the results. The complex wavenumbers locations of the three interactive modes (those with Re(k)\mathrm{Re}(k)>0) shown in Fig. 11 are in good agreement with predictions of the three-wave theory of the Pierce model [33, 11].

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Figure 10: TWT made of a serpentine waveguide operating at millimeter waves. (a) Setup used to determine the dispersion relation of the eigenmodes in the hot serpentine SWS based on PIC simulations. The unit cell has period d and two wave ports are located at the two terminations of the serpentine waveguide. The inset shows the electric and magnetic fields in the metallic rectangular waveguide. (b) Dispersion relation showing the cold eigenmodes of the EM wave (black) and the beam line (red). The electron beam has adc voltage of 20 kV and it interacts with a forward EM mode leading to TWT amplification.
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Figure 11: Complex wavenumbers of the eigenmodes in the interactive (hot) electron beam-EM mode in the serpentine SWS in Fig. 10(a), evaluated using PIC simulations, assuming a beam voltage of 2020 kV and current of 0.10.1 A. (a) Complex plane plot of the four complex wavenumbers in the first Brillouin zone, at f=88f=88 GHz. The red crosses represent the four wavenumbers obtained from the transfer matrix 𝐓u,best\mathbf{T}_{u,best} obtained from (9). Blue dots represent different sets of four wavenumbers obtained from different sets of transfer matrices 𝐓u,qijk\mathbf{T}_{u,qijk} obtained from (13) using different combinations of indices q,i,jq,i,j and kk. Both results are in agreement with the Pierce model [33, 11]. (b) Complex wavenumber-frequency dispersion relations (solid lines). The dashed-red line is the wavenumber dispersion of the electron beam’s space-charge wave described by β0=ω/u0\beta_{0}=\omega/u_{0}, whereas the dashed-black line represents the wavenumber of the EM mode in the cold SWS, i.e., assuming no beam-EM interaction. The figures show the three hybrid modes around the synchronization point, i.e., the three modes with wavenumber with positive real part. The mode associated to the solid-red curve is responsible for amplification since Im(k)\mathrm{Im}(k)>0.

In Fig. 11 we show the modal dispersion relation accounting for the EM-beam interaction in the serpentine SWS using 21 frequency points. The hot dispersion diagrams are obtained using the best-approximate solution 𝐓u,𝑏𝑒𝑠𝑡\mathbf{T}_{\mathit{u,best}} of the overdetermined system in (9). As in the previous section, dashed lines represent the two uncoupled systems: the beam line (dashed red) and the EM mode in the cold SWS (dashed black). The electron beam has a dc voltage of V0=20V_{0}=20 kV so the electron beam interacts with the forward EM wave resulting in an eigenmode with positive imaginary part leading to TWT amplification (red curve). We show only the three modes with positive real wavenumber. One wavenumber has positive imaginary part (solid red curve), which is responsible for amplification, whereas the other two modes resulting from the interaction are decaying and unattenuated modes, in agreement with the Pierce model [11]. The gain per unit-cell associated to the mthm^{th} mode is defined as

Gp,m=Pm[(n+1)d]Pm(nd)=e2Im(km)d,G_{p,m}=\frac{P_{m}[(n+1)d]}{P_{m}(nd)}=e^{2\mathrm{Im}(k_{m})d}, (20)

which is equivalent to 20log(e)Im(kmd)20\log(e)\mathrm{Im}(k_{m}d) dB. The imaginary part of the wavenumber of the amplification mode (solid red) is almost constant and equal toIm(kd)0.027π\mathrm{Im}(kd)\approx 0.027\pi in the frequency range from 87 GHz to 89 GHz shown in Fig. 11, because the phase synchronization condition is almost satisfied for the considered frequency band, i.e., βphβ0\beta_{ph}\approx\beta_{0} over the shown band (relative band of 2.2%2.2\% around 8888GHz) in this example. Thus, the gain per period resulting from the amplification mode (solid red) is 20log(e)×0.027π20\log(e)\times 0.027\pi\approx 0.74 dB in this frequency range which is close to the small-signal gain 1 dB reported in [45] that was obtained by simulating the serpentine TWT amplifier at 90 GHz.

A repeatability study is performed by obtaining the dispersion relation for the serpentine hot SWS using two different numbers of unit cells (all other parameters are kept the same for the two TWT configurations as previously described). Indeed, the transfer matrix of the hot SWS unit-cell 𝐓u\mathbf{T}_{u} should not be a function of the used number of unit-cells, therefore, the dispersion relation obtained using different numbers of unit cells should not be affected. In Fig. 12 we show the complex wavenumberscalculated from the unit-cell transfer matrix 𝐓u\mathbf{T}_{u} estimated using data from PIC simulations of two SWSs with N=13N=13 (as in the previous example) and N=15N=15 unit cells. In each case, we plot 37 sets of four wavenumbers obtained from 37 estimated transfer matrices (distinct determined solutions): blue and green dots represent the cases with N=13N=13 and N=15N=15 unit cells, respectively. The plotted sets are the ones associated with the highest 37 determinants of the matrices 𝐰1,qijk\mathbf{w}_{1,qijk} used to determine the unit-cell transfer matrices 𝐓u,qijk\mathbf{T}_{u,qijk} out of the all 126 combinations for the case with N=13N=13 unit cells and 330 combinations for the case with N=15N=15 unit cells . The red and black crosses represent the wavenumbers obtained from the best-approximate solution of the overdetermined system for the cases with N=13N=13 and N=15N=15 unit cells, respectively. The clustering of wavenumbers at 88 GHz in Fig. 12 shows a good agreement between the two cases based on N=13N=13 and N=15N=15 unit cells. In Fig. 12 we compare the dispersion relation obtained based on the best-approximate solution of the overdetermined system (red and black crosses in Fig. 12): solid and dotted curves represent the dispersion obtained from simulating the hot SWS with N=13N=13 and N=15N=15 unit cells, respectively. The figure shows an almost negligible discrepancy between the dispersion diagrams obtained using two SWS lengths.

f

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Figure 12: Repeatability test for obtaining the complex wavenumbers of the eigenmodes in the interactive (hot) electron beam-EM wave system in Fig. 10(a), evaluated using data from PIC simulations of finite-length serpentine SWS structures with N=13N=13 and N=15N=15 unit cells. (a) Complex plane plot of the four complex wavenumbers in the first Brillouin zone, at f=88f=88 GHz. Blue and green dots represent the wavenumbers obtained from the distinct determined solutions using N=13N=13 and N=15N=15 unit cells, respectively. Whereas the red and black crosses represent the wavenumbers obtained from the best-approximate solution of the overdetermined system using N=13N=13 and N=15N=15 unit cells, respectively. (b) Complex wavenumber-frequency dispersion relations obtained from the best-approximate solution 𝐓u,best\mathbf{T}_{u,best}of the overdetermined system (9) (red and black crosses in (a)). Solid and dotted curves represent the dispersion obtained from the simulation of the finite-length SWS with N=13N=13 and N=15N=15 unit cells, respectively.

V Conclusion

A TWT eigenmode solver to determine the complex wavenumbers of the hybrid eigenmodes in hot SWSs (i.e., accounting for the interaction of the electron beam and the EM wave) has been demonstrated using a novel approximate technique based on data obtained from PIC simulations. The technique has been able to predict the growing mode’s complex wavenumber in both TWTs studied here based on: (i) a SWS made of a circular waveguide with a helix working in the GHz range; (ii) a SWS made of a serpentine waveguide for millimeter wave amplification. The method is based on elaborating the data obtained from time domain PIC simulations, hence accounting for the precise waveguide geometry, materials, losses, and beam space charge effects. We believe that the proposed technique is a powerful tool for the understanding and the design of TWTs amplifiers.

In the present investigation we have focused on determining the complex wavenumbers of the hybrid EM-beam modes, but the same technique can also be used to estimate the performance of longer TWTs based on simulations of shorter TWTs, i.e., it can be used in the design and initial optimization of TWTs. The determination of wavenumbers and eigenvectors of all the hybrid modes supported in a TWT amplifiers discussed here can also be useful to study mode degeneracy conditions in hot SWSs as those investigated in [37, 38, 39].

VI Acknowledgment

This material is based upon work supported by the Air Force Office of Scientific Research award number FA9550-18-1-0355 and award number FA9550-20-1-0409. The authors are thankful to DS SIMULIA for providing CST Studio Suite that was instrumental in this study.

Appendix A Helix dispersion relation using an alternative voltage definition and different structure lengths

In this appendix we test how changing the voltage definition impacts the eigenmodes calculations for the TWT made of a helix SWS considered in Sec. III. We also test how changing the length of the simulated TWT impacts the eigenmodes calculations.

A-A Changing voltage definition

The structure we study here has the same helix parameters and length as the one presented in Sec. III. The only difference is that here we define the voltages representing the EM field as the potential differences between each two consecutive helix loops. We show in Fig. 13 the definition and the numbering scheme for voltages and currents representing the EM and space-charge waves,that are used to construct the circuit network model of each unit-cell. Note that although the structure has 15 periods but it is modeled using 14 network unit-cells because the new voltage definition involve two loops of the helix as shown in Fig. 13.

Theoretically, changing the voltage definition should not impact the eigenvalues, i.e., the determination of the hot SWS modal wavenumbers, however, it affects the calculation of the eigenvectors of the system. We show in Fig. 13 and Fig. 13 the the four complex modal wavenumbers of the hot EM-electron beam system, versus frequency and beam voltage, respectively. The small discrepancy between the wavenumber obtained in Sec. III and the one obtained here based on a different voltage definition may be explained considering the electron beam non-linearity and the change of the beam kinetic voltage along the TWT, in addition to the errors due to finite mesh and finite number of charged particles used to model the TWT dynamics.

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Figure 13: (a) Setup used to determine the frequency-wavenumber dispersion relation assuming the EM waves to be represented using voltages between each two successive loops. Hot dispersion diagram for the four complex wavenumbers versus: (b) frequency using an electron beam with 33 kV and 7575 mA, and (c) electron beam dc kinetic voltage at constant frequency f=4f=4 GHz and dc current of 7575 mA.

A-B Changing the SWS length

We study the effect of changing the simulated TWT length on the calculation of the four complex wavenumbers calculated from the transfer matrix 𝐓u\mathbf{T}_{u} estimated using data from PIC simulations of two SWSs with N=15N=15 and N=17N=17 unit cells. All the used parameters here are kept the same as the ones in Sec. III except that we change the number of the helix SWS unit cells to be N=17N=17, instead of N=15N=15. In Fig. 14 we show the complex wavenumbers. In each case, we plot 75 sets of four wavenumbers obtained from 75 estimated transfer matrices (distinct determined solutions):blue and green dots represent the cases with N=15N=15 and N=17N=17 unit cells, respectively. The plotted sets are the ones associated with the highest 75 determinants of the matrices 𝐰1,qijk\mathbf{w}_{1,qijk} used to determine the unit-cell transfer matrices 𝐓u,qijk\mathbf{T}_{u,qijk} out of the all 330 and 715 combinations for the case with N=15N=15 and N=17N=17 unit cells, respectively. Red and black crosses represent the wavenumbers obtained from the best-approximate solution of the overdetermined system for the cases with N=13N=13 and N=15N=15 unit cells, respectively. The clustering around distinct wavenumbers is consistent when considering the two SWS lengths. The small but noticeable discrepancy in values between the wavenumbers clustering for both cases may be explained as the result of the electron beam non-linearity and other factors like the electron beam loss of energy along the SWS.

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Figure 14: Repeatability test for obtaining the complex wavenumbers of the eigenmodes in the interactive (hot) helix SWS evaluated using data from PIC simulations for finite structures with number of unit-cells N=15N=15 (blue dots) and N=17N=17 (green dots) at f=4f=4 GHz. . The blue and green dots represent the wavenumbers obtained from the distinct determined solutions using N=15N=15 and N=17N=17 unit cells, respectively. Whereas, the red and black crosses represent the wavenumbers obtained from the best-approximate solution of the overdetermined system using N=15N=15 and N=17N=17 unit cells, respectively.

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