Practical predefined-time barrier function-based adaptive sliding mode control for reusable launch vehicle

Author:

Xu Shihao,Guan Yingzi,Bai Yuliang,Wei Changzhu

Funder

Shanghai Academy of Spaceflight Technology

School of Aerospace Science and Technology

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference46 articles.

1. Launch vehicle attitude control using sliding mode control and observation techniques;Stott;J. Franklin Inst. B,2012

2. Finite-time reentry attitude control based on adaptive multivariable disturbance compensation;Tian;IEEE Trans. Ind. Electron.,2015

3. B. Tian, Z. Li, X. Zhao, Q. Zong, Adaptive Multivariable Reentry Attitude Control of RLV with Prescribed Performance, IEEE Trans Syst , Man, Cybern , Syst.

4. 2009 International Conference on Mechatronics and Automation;Cui,2009

5. Adaptive sliding mode control for re-entry attitude of near space hypersonic vehicle based on backstepping design;Zhang;IEEE/CAA J Autom Sinica,2015

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