Fuel Optimal Control of Plane Oscillations of a Satellite on Elliptical Orbit

被引:0
|
作者
Babadzanjanz, Levon [1 ]
Pototskaya, Irina [1 ]
Alesova, Irina [1 ]
Saakyan, Artur [1 ]
机构
[1] St Petersburg State Univ, 7-9 Univ Skaya Nab, St Petersburg 199034, Russia
关键词
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Active damping of the free plane oscillations of a satellite on elliptical orbit is discussed. Satellite oscillations are described by Whittaker-Hill equation. Fuel optimal control method is offered. Numerical examples are submitted.
引用
收藏
页码:82 / 85
页数:4
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