Output feedback attitude control for rigid spacecraft under attitude constraints | Zendy

Tao Guan | Zendy; Bin Li | Zendy

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Output feedback attitude control for rigid spacecraft under attitude constraints

Author(s) -

Tao Guan,

Bin Li

Publication year - 2022

Publication title -

journal of industrial and management optimization

Language(s) - Uncategorized

Resource type - Journals

SCImago Journal Rank - 0.325

H-Index - 32

eISSN - 1553-166X

pISSN - 1547-5816

DOI - 10.3934/jimo.2022173

Subject(s) - quaternion , angular velocity , control theory (sociology) , attitude control , spacecraft , lyapunov function , filter (signal processing) , function (biology) , computer science , sylvester's law of inertia , inertia , rotation matrix , control moment gyroscope , sign function , control (management) , stability (learning theory) , mathematics , physics , nonlinear system , symmetric matrix , control engineering , engineering , artificial intelligence , mathematical analysis , biology , geometry , classical mechanics , quantum mechanics , evolutionary biology , machine learning , computer vision , eigenvalues and eigenvectors , astronomy

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