固体火箭技术2016，Vol.39Issue(5)：715-722,8.DOI:10.7673/j.issn.1006-2793.2016.05.021
基于自适应鲁棒反演的固体动能拦截器姿态跟踪控制
Attitude tracking of KKV based on adaptive backstepping sliding mode control
摘要
Abstract
Aiming at the problem of exo⁃atmospheric kinetic kill vehicle ( KKV) attitude tracking with the characters of con⁃stant thrust, nonlinearity, strong couplings and parameter uncertainties, a novel sliding mode controller was designed which is based on adaptive backstepping theory. The attitude coupling mode was established which considered about interaction between three chan⁃nels and control torque in control loop. The actual control laws and virtual control laws were derived based on the design procedures of sliding mode control and backstepping control, respectively. An adaptive method was introduced to estimate and compensate the model couplings and uncertainties, which improved the accuracy of altitude control. The pulse control laws which could be used for attitude control directly, were calculated from the continuous laws with PWPF modulation. The simulation results show that attitude tracking still satisfies requirements with parameters and disturbance uncertainties.关键词
动能拦截器/变推力控制/PWPF调制器/不确定性Key words
kinetic kill vehicle/thrust variable control/PWPF modulator/uncertainty分类
航空航天引用本文复制引用
杨旭,姚晓先,张皎,刘源翔..基于自适应鲁棒反演的固体动能拦截器姿态跟踪控制[J].固体火箭技术,2016,39(5):715-722,8.基金项目
国家高技术研究发展计划资助项目；国家“985”工程三期重点建设项目。 （）
