Robust attitude tracking control for a rigid spacecraft under input delays and actuator errors
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Publication:5382626
DOI10.1080/00207179.2017.1385855zbMath1416.93059OpenAlexW2766872363MaRDI QIDQ5382626
Hamed Kharrati, Mehdi Baradaran-Nia, Alireza Safa, Sohrab Khanmohammadi
Publication date: 18 June 2019
Published in: International Journal of Control (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1080/00207179.2017.1385855
Related Items (4)
Handling actuator magnitude and rate saturation in uncertain over-actuated systems: a modified projection algorithm approach ⋮ Time‐varying sliding mode controller for over‐actuated systems with constrained and uncertain actuators in flight control applications ⋮ Fault‐tolerant spacecraft attitude control under actuator saturation and without angular velocity ⋮ Chebyshev neural network-based attitude-tracking control for rigid spacecraft with finite-time convergence
Uses Software
Cites Work
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