Fixed-time extended state observer based non-singular fast terminal sliding mode control for a VTVL reusable launch vehicle-Reference-Cited by-同舟云学术

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Fixed-time extended state observer based non-singular fast terminal sliding mode control for a VTVL reusable launch vehicle

Published:2018-11 Issue: Volume:82-83 Page:70-79
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Zhang Liang^ORCID,Wei Changzhu,Wu Rong^ORCID,Cui Naigang^ORCID

Funder

National Natural Science Foundation of China

Fund of National Defense Key Discipline Laboratory of Micro-Spacecraft Technology

Fundamental Research Funds for the Central Universities

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference40 articles.

1. Development and key technologies of vertical takeoff vertical landing reusable launch vehicle;Cui;Astronaut. Syst. Eng. Technol.,2017

2. Adaptive-gain fast super-twisting sliding mode fault tolerant control for a reusable launch vehicle in reentry phase;Zhang;ISA Trans.,2017

3. Fault tolerant attitude control for rigid spacecraft;Li;IEEE Trans. Aerosp. Electron. Syst.,2017

4. Reusable launch vehicle control in multiple-time-scale sliding modes;Shtessel;J. Guid. Control Dyn.,2000

5. Rigid spacecraft attitude control using adaptive non-singular fast terminal sliding mode;Tiwari;J. Control Autom. Electr. Syst.,2015

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