Rigid spacecraft robust optimal attitude stabilization under actuator misalignments-Reference-Cited by-同舟云学术

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Rigid spacecraft robust optimal attitude stabilization under actuator misalignments

Published:2020-10 Issue: Volume:105 Page:105990
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Wang Zhong,Li Yan

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference50 articles.

1. Nonlinear disturbance observer-based robust control for spacecraft formation flying;Lee;Aerosp. Sci. Technol.,2018

2. A novel three-axis attitude stabilization method using in-plane internal mass-shifting;He;Aerosp. Sci. Technol.,2019

3. Robust saturated finite-time attitude control for spacecraft using integral sliding mode;Guo;J. Guid. Control Dyn.,2018

4. Observer-based fault tolerant control and experimental verification for rigid spacecraft;Hu;Aerosp. Sci. Technol.,2019

5. Inverse dynamics particle swarm optimization applied to constrained minimum-time maneuvers using reaction wheels;Spiller;Aerosp. Sci. Technol.,2018

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