Attitude control algorithms for a descent vehicle returning from the moon

被引：0
|
作者：
S. N. Evdokimov
S. I. Klimanov
A. N. Korchagin
E. A. Mikrin
Yu. G. Sikharulidze
A. G. Tuchin
机构：
[1] Russian Academy of Sciences,Keldysh Institute of Applied Mathematics
[2] Korolev Rocket and Space Corporation Energia,undefined
来源：
Journal of Computer and Systems Sciences International | 2017年 / 56卷
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学科分类号：
摘要：
We consider the problem of attitude control of a descent vehicle in the Earth’s atmosphere returning from the Moon. A stabilization algorithm with a deadband and the optimal parameters, obtained with the numerical method, provide adequate landing accuracy and an allowable load factor under the influence of a set of disturbances. Using the method of mathematical simulation, it is shown that the fuel consumption is reduced by ~30% in comparison with the initial stabilization parameters for the descent from a near-Earth orbit.
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页码：483 / 491
页数：8
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