Control Of Spacecraft Subject To Actuator Failures: State-Of-The-Art And Open Problems

this paper we review the main results in the area of active control of spacecraft with one actuator failure. We emphasize the qualitative characteristics that make this a challenging control problem. We also present a series of new results that solve the problems of detumbling with simultaneous attitude stabilization about the unactuated axis, and the complete attitude stabilization and feasible trajectory generation problems for a spacecraft with one actuator failure. INTRODUCTIO