Hybrid Thrust Optimization Control for Orbit Interception Correction

摘要：

　　This paper considers a hybrid optimization control problem by mixing the low and impulsive (high) thrusts,which is a continuous and fixed-time interval control strategy for impulsive control of the orbit interception correction.Initially the linear system model is established and linearized by two-body equations of motion.The hybrid linear control system is analyzed and control law is obtained by solving hybrid Riccati algebraic equations.Finally,by simulation of a numerical example effectiveness of the method is validated.The results show that the hybrid control method combines the advantages of impulsive and low thrusts,giving comprehensive performance better than the method using impulsive thrust control alone.

关键词： Hybrid Optimization Control Impulsive Control Orbit Interception Correction

作者: Huang Yuancan Chen Dongfang

作者单位: School of Mechatronical Engineering,Beijing Institute of Technology,Beijing 100081

会议类型: 国际会议

会议名称: The 33th Chinese Control Conference第33届中国控制会议

会议地点: 南京

会议语种:英文

页码: 719-723

在线出版日期: 2014-07-28（万方平台首次上网日期，不代表论文的发表时间）