Adaptive backstepping controller and sliding mode controller design for formation flight in Sun

Adaptive backstepping controller and sliding mode controller design for formation flight in Sun–Earth L 2 point

Published:2016-08 Issue: Volume:55 Page:409-418
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Wang Feng,Liu Ming,Jin Rongyu,Li Zhuoshi

Funder

Ministry of Education of China

National Natural Science Foundation of China

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

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference24 articles.

1. A.M. Sergaman, M.F. Zedd, Investigations of spacecraft orbits around the L2 Sun–Earth libration point, Naval Research Report, 2005, NRL/MR8233-05-NRL/MR8233-8897.

2. Adaptive sliding mode control for interval type-2 fuzzy systems;Li;IEEE Trans. Syst. Man Cybern.,2016

3. Robust optimal sliding mode control for spacecraft position and attitude maneuvers;Pukdeboon;Aerosp. Sci. Technol.,2015

4. Output-feedback based sliding mode control for fuzzy systems with actuator saturation;Li;IEEE Trans. Fuzzy Syst.,2015

5. Indirect adaptive control for attitude tracking of spacecraft with unknown reaction wheel friction;Cao;Aerosp. Sci. Technol.,2015

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