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Record Nr. |
UNINA9910743364903321 |
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Autore |
Wang Jie <1275-1336, > |
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Titolo |
Rigid-Flexible Coupling Dynamics and Control of Flexible Spacecraft with Time-Varying Parameters / / by Jie Wang, Dong-Xu Li |
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Pubbl/distr/stampa |
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Singapore : , : Springer Nature Singapore : , : Imprint : Springer, , 2022 |
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ISBN |
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981-16-5097-7 |
981-16-5096-9 |
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Edizione |
[1st ed. 2022.] |
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Descrizione fisica |
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1 online resource (190 pages) |
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Collana |
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Intelligent Technologies and Robotics Series |
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Disciplina |
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Soggetti |
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Automatic control |
Dynamics |
Nonlinear theories |
Aerospace engineering |
Astronautics |
Control and Systems Theory |
Applied Dynamical Systems |
Aerospace Technology and Astronautics |
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Lingua di pubblicazione |
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Formato |
Materiale a stampa |
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Livello bibliografico |
Monografia |
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Nota di contenuto |
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Introduction -- Modeling of Flexible Spacecraft with Time-varying Parameters -- Dynamic Analysis of Flexible Spacecraft with Time-varying Parameters -- Vibration Control Methods for Systems in Complex Mode Space -- Optimal Variable Amplitudes Input Shaping Control for Slew Maneuver of Flexible Spacecraft -- Coupling Control Method for Flexible Spacecraft -- Attitude Coupling Control Experiments -- Future. |
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Sommario/riassunto |
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This book presents the dynamic modeling and attitude control of flexible spacecraft with time-varying parameters. The dynamic characteristics, vibration control methods and attitude stabilization methods for spacecraft are systematically studied in respects of the theoretical modeling, numerical simulation and the ground experiment. Three active control theories in complex mode space are presented for flexible space structures. Optimal slew strategies based on variable |
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