Numerical Simulation and Kalman-based Control of a Hall Thruster for CubeSats
Keywords:
Electric propulsion, Satellites, Kalman Filter Extended, Particle-In-Cell simulation, Hall thrustersAbstract
This work presents a coupled simulation framework combining a Particle-In-Cell (PIC) model and a Kalman filter-based estimator to evaluate the influence of electric propulsion on CubeSat trajectory control. A three-dimensional PIC simulation of the PHALL II-C Hall thruster was performed using a CAD model developed in SolidWorks and imported into the VSim software. From the PIC simulation, the electric and magnetic fields, electric potential, ion velocity, and thrust (64 mN) were obtained. This thrust value was then used as input for an Extended Kalman Filter (EKF) implemented in MATLAB to simulate the orbital behavior of a 6U CubeSat at 700 km altitude under continuous low-thrust conditions. The filter accurately estimated angular position, altitude, and vertical velocity over time, with low Mean Absolute Error and Root Mean Square Error values across all states. The results demonstrate the effectiveness of combining plasma simulations with state estimation techniques for nano and microsatellite mission analysis.
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