以组合飞行器为研究对象,介绍了组合飞行器在轨服务期间的姿态跟踪控制。利用无源性(输入输出稳定性)控制理论和自适应模糊逻辑系统设计了一种自适应控制方案,该方案利用飞行器的动力学特性以及模糊逻辑系统的万能逼近能力,使得所设计的控制器对飞行器的模型不确定性和外部环境力矩具有很强的自适应性和鲁棒性。 Taking the combination aircraft as the research object, the attitude tracking control of the combination aircraft during the service of the orbit is introduced. An adaptive control scheme is designed by using passive (input / output stability) control theory and adaptive fuzzy logic system. The scheme utilizes the dynamics of aircraft and the universal approximation ability of fuzzy logic system, so that the designed controller It has strong adaptability and robustness to aircraft model uncertainty and external environment torque.