Adaptive Fixed-Time Terminal Sliding Mode Control on SE(3) for Coupled Spacecraft Tracking Maneuver
In this paper, a JOINT-PRO FORMULA reaching law-based adaptive fixed-time terminal sliding mode control law, which is used for coupled spacecraft tracking maneuver in the presence of large inertia parametric uncertainties and external disturbances, is proposed.The coupled 6-DOF kinematics and dynamics for spacecraft motion are modeled on Lie group