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Xiaoyun Sun

Nanjing University of Aeronautics and Astronautics

Yudao Street

210016

Nanjing,, 210016

China

  • Nanjing University of Aeronautics and Astronautics

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Scholarly Papers (1)

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Output Tracking Robust Adaptive Spacecraft Attitude-Orbit Coupled Non-Affine Formation Control for Space Gravitational Wave Detection

Number of pages: 20 Posted: 08 May 2025
Xiaoyun Sun, Qiang Shen and Shufan Wu
Nanjing University of Aeronautics and Astronautics, affiliation not provided to SSRN and Shanghai Jiao Tong University (SJTU)
Downloads 25 (1,385,945)

Abstract:

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consensus control, model reference adaptive control, output regulation, attitude-orbit dynamics, linear matrix inequalities, non-affine control, robust control