FURTHER RESULTS ON THE OPTIMAL REGULATION OF SPACECRAFT ANGULAR-MOMENTUM

被引：8
|
作者：
BOURDACHESIGUERDIDJANE, H [1 ]
机构：
[1] UNIV MUNICH,INST MATH,W-8000 MUNICH 2,GERMANY
来源：
OPTIMAL CONTROL APPLICATIONS & METHODS | 1991年 / 12卷 / 04期
关键词：
SATELLITE ANGULAR MOMENTUM; NONLINEAR OPTIMAL FEEDBACK LAW; CHARACTERISTIC VALUES; CHARACTERISTIC VECTORS;
D O I：
10.1002/oca.4660120406
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
A direct analytical solution of angular velocities is given for regulating the angular momentum of a spacecraft using reaction jets only. The solution, which appears to be new, may be written down in terms of characteristic values and characteristic vectors. These values and vectors satisfy an algebraic non-linear equation.
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页码：273 / 278
页数：6
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