Optimal Guidance in Atmosphere for Aeroassisted Space Rendezvous

被引：0
|
作者：
Zhou Wenya [1 ]
Yang Di [1 ]
Chen Hongbo
机构：
[1] Harbin Inst Technol, Dept Aerosp Engn, Harbin 150001, Peoples R China
来源：
PROCEEDINGS OF THE 27TH CHINESE CONTROL CONFERENCE, VOL 3 | 2008年
基金：
国家高技术研究发展计划(863计划);
关键词：
Aeroassisted Space Rendezvous; Nominal Guidance; Linear Quadratic Regulator; Robustness;
D O I：
10.1109/CHICC.2008.4605192
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
Aiming at time constraint and trajectory phase angle constraint of aeroassisted space rendezvous, a approach guidance method belonging to the nominal guidance was presented. Due to initial trajectory errors and external disturbances existing in atmospheric flight, linear quadratic regulator was designed and computation method of weighted coefficient matrixes was given. Mathematic simulation example indicated that the designed regulator was strong robustness to the initial trajectory errors and external disturbances.
引用
收藏
页码：506 / +
页数：2
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