Optimal-fuel Control Design of Nonlinear Spacecraft Rendezvous System with the Collision Avoidance Constraint

被引：0
|
作者：
Shao, Lili [1 ]
Liu, Zhongbo [2 ]
Gao, Xiangyu [1 ]
机构：
[1] Heilongjiang Univ, Sch Math Sci, Harbin 150080, Peoples R China
[2] Heilongjiang Univ, Key Construct & Dev Dept, Harbin 150080, Peoples R China
来源：
PROCEEDINGS OF 2015 INTERNATIONAL CONFERENCE ON ESTIMATION, DETECTION AND INFORMATION FUSION ICEDIF 2015 | 2015年
关键词：
Nonlinear system; spacecraft rendezvous; fuel-optimal control; exact penalty function method; state constraint; RECONFIGURATION; MANEUVERS; OPTIMIZATION; ALGORITHM; ORBIT;
D O I：
暂无
中图分类号：
TM [电工技术]; TN [电子技术、通信技术];
学科分类号：
0808 ; 0809 ;
摘要：
This paper studies the optimal-fuel control problem of spacecraft rendezvous with collision avoidance constraint. A nonlinear spacecraft rendezvous model is established. Based on this model, an optimal control problem with state constraint is formulated. An exact penalty function method is used to transform the constrained optimal control problem into a sequence of approximate unconstrained optimization problems. Finally, it is shown that the solutions of these approximate unconstrained optimization problems converge to the solution of the original problem.
引用
收藏
页码：348 / 353
页数：6
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