409,76 €
455,29 €
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Control Allocation for Spacecraft Under Actuator Faults
Control Allocation for Spacecraft Under Actuator Faults
409,76
455,29 €
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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 Contr…
  • Publisher:
  • ISBN-10: 981160441X
  • ISBN-13: 9789811604416
  • Format: 15.6 x 23.4 x 1.3 cm, softcover
  • Language: English
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Control Allocation for Spacecraft Under Actuator Faults (e-book) (used book) | bookbook.eu

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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

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  • Author: Qinglei Hu
  • Publisher:
  • ISBN-10: 981160441X
  • ISBN-13: 9789811604416
  • Format: 15.6 x 23.4 x 1.3 cm, softcover
  • Language: English English

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

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