Control Allocation for Spacecraft Under Actuator Faults

by Qinglei Hu

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Introduction.- Spacecraft Model and Control Allocation Formulation.- Null-space based Optimal Control Allocation for Spacecraft Stabilization.- Robust finite-time control allocation under actuator misalignment.- Finite-Time Fault-Tolerant Spacecraft Attitude Control and Control allocation with Torque Saturation.- Fault Tolerant Control Allocation of Spacecraft Using Fault Detection and Diagnosis.- Extended State Observer based Optimal Control Allocation.- Nonlinear Proportional-Derivative Control Incorporating Closed-loop Control Allocation.- Closed-Loop-Based Control Allocation for Spacecraft Attitude Stabilization with Actuator Fault.- Conclusion

Format:Paperback

Language:English

ISBN:981160441X

ISBN13:9789811604416

Release Date:March 2022

Publisher:Springer

Length:221 Pages

Weight:0.75 lbs.

Dimensions:0.5" x 6.1" x 9.2"

Related Subjects

Engineering Technology

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Control Allocation for Spacecraft Under Actuator Faults

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