Angular motion equations for a satellite with hinged flexible solar panel

Author:

Ovchinnikov M.Yu.,Tkachev S.S.,Roldugin D.S.,Nuralieva A.B.,Mashtakov Y.V.

Funder

Russian Science Foundation

Publisher

Elsevier BV

Subject

Aerospace Engineering

Cited by 11 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Attitude Stabilization of a Satellite with Large Flexible Elements Using On-Board Actuators Only;Mathematics;2023-12-11

2. Distributed Vibration Control of Large Flexible Satellite Solar Panel Via Reinforcement Learning;2023 35th Chinese Control and Decision Conference (CCDC);2023-05-20

3. Mathematical Model of a Satellite with an Arbitrary Number of Flexible Appendages;Mathematical Models and Computer Simulations;2021-07

4. Optimizing Magnification Ratio for the Flexible Hinge Displacement Amplifier Mechanism Design;Proceedings of the 2nd Annual International Conference on Material, Machines and Methods for Sustainable Development (MMMS2020);2021

5. Математическая модель спутника с произвольным числом нежестких элементов;Математическое моделирование;2020-11-16

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