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Record Nr. |
UNINA9910739412403321 |
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Autore |
Hu Qinglei |
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Titolo |
Control allocation for spacecraft under actuator faults / / Qinglei Hu [et al.] |
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Pubbl/distr/stampa |
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Singapore : , : Springer, , [2021] |
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©2021 |
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ISBN |
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Descrizione fisica |
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1 online resource (xviii, 221 pages) |
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Disciplina |
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Soggetti |
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Space vehicles - Attitude control systems |
Actuators |
Vehicles espacials |
Actuadors |
Sistemes adaptatius |
Llibres electrònics |
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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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Intro -- Preface -- Acknowledgements -- Contents -- Acronyms -- 1 Introduction -- 1.1 Background and Motivations -- 1.2 Introduction to Control Allocation -- 1.2.1 Control Allocation Methods -- 1.2.2 Applications of Control Allocation in Aeronautics and Astronautics -- 1.3 Introduction to Fault-Tolerant Control -- 1.3.1 Fault-Tolerant Control Methods -- 1.3.2 Applications of Fault-Tolerant Control in Aeronautics and Astronautics -- 1.4 Organization of the Book -- References -- 2 Mathematical Model of the Attitude Control System -- 2.1 Spacecraft Attitude Kinematics -- 2.1.1 Euler Angles Based Model -- 2.1.2 Quaternion Based Model -- 2.1.3 Modified Rodrigues Parameters Based Model -- 2.2 Spacecraft Attitude Dynamics Model -- References -- 3 Null-Space Based Optimal Control Allocation for Spacecraft Attitude Stabilization -- 3.1 Introduction -- 3.2 Problem Formulation -- 3.2.1 Spacecraft Attitude Dynamics -- 3.2.2 Control Objective -- 3.3 Attitude Control Law Design -- 3.3.1 SPD-Based Virtual/Baseline Control Law Design -- 3.3.2 Null-Space-Based Optimal Control Reallocation Scheme -- 3.4 Simulation Results -- 3.4.1 Time |
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