Adaptive terminal sliding mode control for satellite formation flying system with external disturbance and actuator misalignment

In this paper, the distributed attitude synchronization control problem is addressed for satellite formation flying system (SFFS) with external disturbance and actuator misalignment by using adaptive terminal sliding mode control (ATSMC) technique. The satellite attitude system model considered in this paper is transformed into a lagrange nonlinear system. On this basis, a terminal sliding mode surface is designed for the attitude tracking error...