飞控与探测2025，Vol.8Issue(5)：44-52,9.DOI:10.20249/j.cnki.2096-5974.2025.05.005
应用控制力矩陀螺卫星的事件触发式姿态机动预测控制器设计
Design of Event-Triggered Attitude Maneuver Predictive Controller for Application Control Moment Gyroscope Satellite
摘要
Abstract
In response to the singular phenomena that are prone to occur during attitude maneuvers of the application control moment gyroscope(CMG)satellites,an attitude dynamics equation is established with CMG speed commands as input.The established state space equation is dis-cretized,and optimization calculation indicators are designed.Online optimization calculation of input speed commands is used to minimize torque errors caused by commonly used CMG control laws.A predictive control algorithm based on optimization iteration is designed to provide an atti-tude maneuver feedback controller with a closed-loop structure.In order to reduce the computa-tional burden of online optimization and minimize the number of optimization calculations,a satel-lite attitude maneuver predictive controller with an event-triggered mechanism is designed,the controller can avoid CMG singularity and control satellite rapid maneuver,and effectively reduces the burden of in-orbit calculation on this basis.Through the simulation of the event-triggered atti-tude maneuver prediction controller for rigid body satellites,it is further demonstrated that this controller has the remarkable ability to significantly reduce the online computing burden.关键词
事件触发/卫星姿态机动/模型预测控制/控制力矩陀螺Key words
event-triggered/satellite attitude maneuver/model predictive control/control moment gyro-scope分类
航空航天引用本文复制引用
梁田宏,刘刚,朱文山..应用控制力矩陀螺卫星的事件触发式姿态机动预测控制器设计[J].飞控与探测,2025,8(5):44-52,9.基金项目
上海航天科技创新基金(SAST2022-79) （SAST2022-79）
