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DESATURATION METHOD FOR ACCUMULATED ACTUATOR MOMENTUM OF THE SPACECRAFT ON HIGH-ELLIPTIC ORBIT IN ROLL AND YAW CHANNELS
Vorobyeva Ekaterina Andreevna
S.P. Korolev Rocket and Space Public Corporation Energia
S.P. Korolev Rocket and Space Public Corporation Energia
Abstract
The development of the attitude control algorithm while regulating the accumulated angular momentum inertial actuator or the spacecraft on high-elliptical orbit in the area of the orbit-free performance targets is considered.
Keywords: gravity gradient forces, high-elliptic orbit, inertial actuator, MIMO-system? инерционные исполнительные органы, spacecraft
Category: 05.00.00 Technical sciences
Article reference:
Desaturation method for accumulated actuator momentum of the spacecraft on high-elliptic orbit in roll and yaw channels // Modern scientific researches and innovations. 2015. № 11 [Electronic journal]. URL: https://web.snauka.ru/en/issues/2015/11/59141
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