平均法在微倾斜轨道卫星洛伦兹稳定问题中的应用

2020 15th International Conference on Stability and Oscillations of Nonlinear Control Systems (Pyatnitskiy's Conference) (STAB) Pub Date : 2020-06-01 DOI:10.1109/STAB49150.2020.9140567

A. Aleksandrov, A. Tikhonov

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引用次数: 1

摘要

研究了在扰动重力力矩作用下，小倾角轨道上卫星在轨道坐标系中的洛伦兹稳定问题。为了解决这一具有不完全控制特征的问题，提出了微分方程的平均技术。使用了李雅普诺夫函数的原始构造。

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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On the Application of the Averaging Method in the Problem of Lorentz Stabilization of a Satellite on a Slightly Inclined Orbit

The problem of Lorentz stabilization of a satellite in the orbital coordinate system on an orbit of small inclination under conditions of a disturbing gravitational torque is studied. To solve this problem, which is characterized by incomplete control, the averaging technique for differential equations is developed. An original construction of a Lyapunov function is used.

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来源期刊

2020 15th International Conference on Stability and Oscillations of Nonlinear Control Systems (Pyatnitskiy's Conference) (STAB)

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