OPTIMAL REORIENTATION OF A SATELLITE ON A CIRCULAR ORBIT.

被引：0

作者：

Anchev, A.A.

Melikyan, A.A.

机构：

来源：

Mechanics of solids | 1980年 / 15卷 / 06期

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中图分类号：

V4 [航天（宇宙航行）];

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摘要：

This article considers the problem of optimal control of a mathematical pendulum, which also describes controlled rotation of a satellite in the plane of a circular orbit. A numerical and qualitative investigation of the programmed problem of reorientation of a satellite is carried out for small values of the control moment, and the response time and number of switching as functions of the moment is plotted.

引用

页码：28 / 32