Fuel optimal control of plane oscillations of a satellite on elliptical orbit

2015 International Conference "Stability and Control Processes" in Memory of V.I. Zubov (SCP) Pub Date : 2015-12-03 DOI:10.1109/SCP.2015.7342062

L. Babadzanjanz, I. Pototskaya, I. Alesova, A. Saakyan

引用次数: 10

Abstract

Active damping of the free plane oscillations of a satellite on elliptical orbit is discussed. Satellite oscillations are described by Whittaker-Hill equation. Fuel optimal control method is offered. Numerical examples are submitted.

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椭圆轨道卫星平面振荡的燃料最优控制

讨论了椭圆轨道卫星自由平面振动的主动阻尼问题。卫星振荡用惠特克-希尔方程描述。提出了燃油最优控制方法。给出了数值算例。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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来源期刊

2015 International Conference "Stability and Control Processes" in Memory of V.I. Zubov (SCP)

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