Unloading Angular Momentum for Inertial Actuators of a Spacecraft in the Pitch Channel

被引：10
|
作者：
Bogachev, A. V. [1 ]
Vorob'eva, E. A. [1 ]
Zubov, N. E. [1 ]
Mikrin, E. A. [1 ]
Misrikhanov, M. Sh. [1 ]
Ryabchenko, V. N. [1 ]
Timakov, S. N. [1 ]
机构：
[1] SP Korolev Rocket & Space Corp Energiya, Korolev, Russia
来源：
JOURNAL OF COMPUTER AND SYSTEMS SCIENCES INTERNATIONAL | 2011年 / 50卷 / 03期
关键词：
Angular Momentum; System Science International; Elliptic Orbit; Gain Coefficient; Gravitational Moment;
D O I：
10.1134/S1064230711030075
中图分类号：
TP18 [人工智能理论];
学科分类号：
081104 ; 0812 ; 0835 ; 1405 ;
摘要：
The problem of gravitational unloading of the angular momentum of inertial actuators of a spacecraft in the pitch channel for circular and elliptic orbits is considered using the band theory of modal control. Control laws for gravitational unloading and stabilization of a given spacecraft position unambiguously determined by the object parameters and given coefficients of characteristic equation are obtained.
引用
收藏
页码：483 / 490
页数：8
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