Titlebook: Control Allocation for Spacecraft Under Actuator Faults; Qinglei Hu,Bo Li,Youmin Zhang Book 2021 The Editor(s) (if applicable) and The Aut

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著名

Control Allocation for Spacecraft Under Actuator Faults978-981-16-0439-3

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果仁

極肥胖

Nonlinear Proportional-Derivative Control Incorporating Closed-Loop Control Allocation for Spacecraiscrepancies or saturation phenomenon may reduce the control system performances and even cause the instability of the whole control system if it could be well handled and solved. All of the above mentioned problems cause considerable difficulties and challenges in the spacecraft ACS design, for mee

胰島素

Closed-Loop Based Control Allocation for Spacecraft Attitude Stabilization with Actuator Faults,ve SMC law to dynamically compensate the perturbations due to actuator faults and other uncertainties, in which the real time CA algorithm delivers the control command to actuators. In [.], a novel dynamic near-optimal CA scheme with combination of a saturated baseline controller for spacecraft atti

胰島素

外來

Closed-Loop Based Control Allocation for Spacecraft Attitude Stabilization with Actuator Faults,be degraded, even the unstable ACS may result in the completely collapse, immeasurable losses or catastrophic consequences. Thus, the spacecraft ACS should be capable of dealing with or tolerating possible actuator faults, while at the same time guaranteeing an acceptable performance in the presence

BOOR

Qinglei Hu,Bo Li,Youmin ZhangPresents the existing and emerging concepts concerning control allocation, and attitude control and fault-tolerant control for the over-actuated spacecraft under actuator failures.Addresses the resear

領(lǐng)帶

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