Control of a Thrust-Vectoring CubeSat Using a Single Variable-Speed Control Moment Gyroscope

Author:

Biggs James D.1,Livornese Gaetano1

Affiliation:

1. Polytechnic of Milan, 20133 Milan, Italy

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Cited by 5 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. Prescribed-time attitude control during solid thrusting orbital maneuver;2022 IEEE 17th Conference on Industrial Electronics and Applications (ICIEA);2022-12-16

2. A prescribed time attitude control method based on thrust vector control (TVC) nozzle for solid propulsion satellite;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-11-25

3. Genetic Algorithm Based Sliding Mode Controller for Underactuated 2-DoF Gyroscope;Control and Measurement Applications for Smart Grid;2022

4. Robust spacecraft rendezvous using a variable speed control moment gyro and thruster;Aerospace Science and Technology;2021-05

5. Disturbance Observer-Based Nonsingular Terminal Sliding Mode Control for Spacecraft Electromagnetic Docking;International Journal of Aerospace Engineering;2020-10-27

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