Fixed-time attitude tracking control for spacecraft without unwinding-Reference-Cited by-同舟云学术

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Fixed-time attitude tracking control for spacecraft without unwinding

Published:2018-10 Issue: Volume:151 Page:818-827
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Huang Bing,Li Ai-jun,Guo Yong,Wang Chang-qing

Funder

Shaanxi Province Key Laboratory of flight control and Simulation Technology

the Fundamental Research Funds for the Central Universities

Aeronautical Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference32 articles.

1. Adaptive relative pose control of spacecraft with model couplings and uncertainties;Sun;Acta Astronaut.,2018

2. Robust reliable control for autonomous spacecraft rendezvous with limited-thrust;Yang;Aero. Sci. Technol.,2013

3. Earth observation from the manned low Earth orbit platforms;Guo;ISPRS J. Photogrammetry Remote Sens.,2016

4. A hybrid online scheduling mechanism with revision and progressive techniques for autonomous Earth observation satellite;Li;Acta Astronaut.,2017

5. Attitude coordination of multiple spacecraft for space debris surveillance;Felicetti;Adv. Space Res.,2017

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