Nonlinear Robust H∞ Control for Spacecraft Body-Fixed Hovering Around Noncooperative Target Via Modified θ - D Method

This paper addresses the robust control problem of spacecraft body-fixed hovering near a noncooperative target in the presence of parametric uncertainties and disturbances. A closed-form nonlinear robust H-infinity controller constructed by the solution of Hamilton-Jacobi-Isaacs (HJI) inequality is designed, which can stabilize the closed-loop system with the H-infinity performance. To obtain the solution of HJI, an effective numerical approximation approach called the modified theta-D method is proposed, which can obtain a numerical approximation solution of HJI by only solving one algebraic Riccati inequality and several Lyapunov equations rather than a partial differential inequality. The detailed numerical calculation processes of solving the HJI are presented, which shows that the modified theta-D method can be implemented offline with less computational burden. Finally, the effectiveness of the designed robust control scheme is demonstrated via a numerical example.