Adaptive prediction backstepping attitude control for liquid-filled micro-satellite with flexible appendages

Author:

Huo Jun-hai,Meng Tao,Song Ren-ting,Jin Zhong-he

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference25 articles.

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5. Orbit insertion dynamics of a pico-satellite with respect to coupled solid-liquid dynamics;Baeten,2013

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