Pulse-Width Predictive Control for LTV Systems with Application to Spacecraft Rendezvous
Provides a computationally efficient MPC method for LTV systems with PWM actuators, relevant to aerospace control.
The paper develops an MPC for LTV systems with PWM control, using a planner with PAM/impulsive hot-start and linearization for fast solution improvement. Simulation on spacecraft rendezvous in eccentric orbits demonstrates efficacy.
This work presents a model predictive controller (MPC) that is able to handle linear time-varying (LTV) plants with PWM control. The MPC is based on a planner that employs a PAM or impulsive approximation as a hot-start and then uses explicit linearization around successive PWM solutions for rapidly improving the solution by means of linear programming. As an example, the problem of rendezvous of spacecraft for eccentric target orbits is considered. The problem is modeled by the LTV Tschauner-Hempel equations, whose transition matrix is explicit; this is exploited by the algorithm for rapid convergence. The efficacy of the method is shown in a simulation study.