Prescribed performance based adaptive model-free control for highly flexible spacecraft detumbling rotating satellites
Author:
Funder
National Key Research and Development Program of China
National Natural Science Foundation of China
Publisher
Elsevier BV
Reference37 articles.
1. Finite-time fault tolerant attitude tracking control of spacecraft using robust nonlinear disturbance observer with anti-unwinding approach;Amrr;Adv. Space. Res.,2020
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3. Non-fragile tracking control of constrained waverider vehicles with readjusting prescribed performance;Bu;Nonlinear Dyn.,2022
4. Accurate dynamic modeling of detumbling rotating satellites with large flexible solar panels;Chen;Adv. Space. Res.,2023
5. Optimal nutation suppressing method for detumbling satellites via a flexible deceleration device;Chen;Nonlinear Dyn.,2023
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