Abstract: This paper investigates the problem of robust guaranteed cost output tracking control for the homing phase of spacecraft rendezvous. Based on the Clohessy-Wiltshire (C-W) equations, and by simultaneously considering the ...

Abstract: Based on the nonlinear stable inversion approach, an exact output tracking control law is designed for flexible air-breathing hypersonic vehicles (FAHVs). This problem is challenging because of the inherent couplings between ...