Synthesis of Attitude Control for a Gyroscopic Stabilizer of the Navigation System of a Descent Vehicle

被引：0
|
作者：
S. V. Sokolov
V. A. Pogorelov
机构：
[1] Rostov Military Institute of Missile Troops,
来源：
Cosmic Research | 2001年 / 39卷
关键词：
State Vector; Control Vector; Attitude Control; Navigation System; Analytical Form;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
The possibility to synthesize the attitude control for a gyrostabilized platform is investigated under the most general assumptions on its drifts, using the principle of maximum. The analytical form of the control vector, explicitly depending on all components of the state vector of a navigation system of a descent vehicle, is a specific feature of the found solution.
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收藏
页码：498 / 503
页数：5
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