Attitude Stabilization of Spacecraft Using Variable Step-Size Pulse-Width-Modulated Thrusters

Authors :: Xiaowei Zhang
Shuang Li
Bingheng Wang
Beichao Wang
Source :: Journal of Guidance, Control, and Dynamics. 45:376-384
Publication Year :: 2022
Publisher :: American Institute of Aeronautics and Astronautics (AIAA), 2022.

Subjects :: Closed-loop transfer function
Physics
Spacecraft
business.industry
Applied Mathematics
Describing function
Aerospace Engineering
Space and Planetary Science
Control and Systems Engineering
Control theory
Fuel efficiency
Communications satellite
Electrical and Electronic Engineering
Orbital maneuver
business
Bang–bang control
Variable (mathematics)

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