Control Allocation for Spacecraft Under Actuator Faults
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Published By Springer Singapore

9789811604386, 9789811604393

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Mathematical Model of the Attitude Control System

Control Allocation for Spacecraft Under Actuator Faults ◽

10.1007/978-981-16-0439-3_2 ◽

2021 ◽

pp. 23-31

Author(s):

Qinglei Hu ◽

Bo Li ◽

Bing Xiao ◽

Youmin Zhang

Keyword(s):

Mathematical Model ◽

Control System ◽

Attitude Control ◽

Attitude Control System

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Extended State Observer Based Optimal Attitude Robust Control of Spacecraft

Control Allocation for Spacecraft Under Actuator Faults ◽

10.1007/978-981-16-0439-3_6 ◽

2021 ◽

pp. 109-131

Author(s):

Qinglei Hu ◽

Bo Li ◽

Bing Xiao ◽

Youmin Zhang

Keyword(s):

Robust Control ◽

State Observer ◽

Extended State Observer ◽

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Conclusions

Control Allocation for Spacecraft Under Actuator Faults ◽

10.1007/978-981-16-0439-3_10 ◽

2021 ◽

pp. 219-221

Author(s):

Qinglei Hu ◽

Bo Li ◽

Bing Xiao ◽

Youmin Zhang

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Introduction

Control Allocation for Spacecraft Under Actuator Faults ◽

10.1007/978-981-16-0439-3_1 ◽

2021 ◽

pp. 1-22

Author(s):

Qinglei Hu ◽

Bo Li ◽

Bing Xiao ◽

Youmin Zhang

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Nonlinear Proportional-Derivative Control Incorporating Closed-Loop Control Allocation for Spacecraft

Control Allocation for Spacecraft Under Actuator Faults ◽

10.1007/978-981-16-0439-3_8 ◽

2021 ◽

pp. 157-183

Author(s):

Qinglei Hu ◽

Bo Li ◽

Bing Xiao ◽

Youmin Zhang

Keyword(s):

Closed Loop ◽

Control Allocation ◽

Closed Loop Control ◽

Loop Control ◽

Derivative Control

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Robust Finite-Time Control Allocation for Attitude Stabilization Under Actuator Misalignment

Control Allocation for Spacecraft Under Actuator Faults ◽

10.1007/978-981-16-0439-3_4 ◽

2021 ◽

pp. 55-71

Author(s):

Qinglei Hu ◽

Bo Li ◽

Bing Xiao ◽

Youmin Zhang

Keyword(s):

Finite Time ◽

Control Allocation ◽

Attitude Stabilization ◽

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Closed-Loop Based Control Allocation for Spacecraft Attitude Stabilization with Actuator Faults

Control Allocation for Spacecraft Under Actuator Faults ◽

10.1007/978-981-16-0439-3_9 ◽

2021 ◽

pp. 185-217

Author(s):

Qinglei Hu ◽

Bo Li ◽

Bing Xiao ◽

Youmin Zhang

Keyword(s):

Closed Loop ◽

Control Allocation ◽

Spacecraft Attitude ◽

Actuator Faults ◽

Attitude Stabilization

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Finite-Time Fault-Tolerant Spacecraft Attitude Control with Torque Saturation

Control Allocation for Spacecraft Under Actuator Faults ◽

10.1007/978-981-16-0439-3_5 ◽

2021 ◽

pp. 73-108

Author(s):

Qinglei Hu ◽

Bo Li ◽

Bing Xiao ◽

Youmin Zhang

Keyword(s):

Finite Time ◽

Attitude Control ◽

Fault Tolerant ◽

Spacecraft Attitude ◽

Spacecraft Attitude Control

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Spacecraft Attitude Fault-Tolerant Control Based on Iterative Learning Observer and Control Allocation

Control Allocation for Spacecraft Under Actuator Faults ◽

10.1007/978-981-16-0439-3_7 ◽

2021 ◽

pp. 133-155

Author(s):

Qinglei Hu ◽

Bo Li ◽

Bing Xiao ◽

Youmin Zhang

Keyword(s):

Fault Tolerant ◽

Fault Tolerant Control ◽

Iterative Learning ◽

Control Allocation ◽

Spacecraft Attitude ◽

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Null-Space Based Optimal Control Allocation for Spacecraft Attitude Stabilization

Control Allocation for Spacecraft Under Actuator Faults ◽

10.1007/978-981-16-0439-3_3 ◽

2021 ◽

pp. 33-53

Author(s):

Qinglei Hu ◽

Bo Li ◽

Bing Xiao ◽

Youmin Zhang

Keyword(s):

Optimal Control ◽

Control Allocation ◽

Spacecraft Attitude ◽

Attitude Stabilization

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