摘要
提出以库仑力为主、电推进为辅助的混合推进,用以解决库仑卫星编队在碰撞规避过程中的重构控制问题,重构控制采用模糊最优二次型控制,最后通过仿真进行了验证。
The hybrid propulsion which consists of Coulomb force and electric propulsion is proposed to achieve the reconfiguration control of Coulomb satellite formation during collision avoidance process. In addition,fuzzy LQR control is applied to reconfiguration control by simulations.
出处
《航天控制》
CSCD
北大核心
2017年第2期20-24,共5页
Aerospace Control
关键词
混合推进
库仑卫星编队
碰撞规避
重构控制
Hybrid propulsion
Coulomb satellite formation
Obstacle avoidance
Reconfiguration control
