commingle 发表于 2025-3-21 16:24:49
书目名称Control Allocation for Spacecraft Under Actuator Faults影响因子(影响力)<br> http://impactfactor.cn/2024/if/?ISSN=BK0237226<br><br> <br><br>书目名称Control Allocation for Spacecraft Under Actuator Faults影响因子(影响力)学科排名<br> http://impactfactor.cn/2024/ifr/?ISSN=BK0237226<br><br> <br><br>书目名称Control Allocation for Spacecraft Under Actuator Faults网络公开度<br> http://impactfactor.cn/2024/at/?ISSN=BK0237226<br><br> <br><br>书目名称Control Allocation for Spacecraft Under Actuator Faults网络公开度学科排名<br> http://impactfactor.cn/2024/atr/?ISSN=BK0237226<br><br> <br><br>书目名称Control Allocation for Spacecraft Under Actuator Faults被引频次<br> http://impactfactor.cn/2024/tc/?ISSN=BK0237226<br><br> <br><br>书目名称Control Allocation for Spacecraft Under Actuator Faults被引频次学科排名<br> http://impactfactor.cn/2024/tcr/?ISSN=BK0237226<br><br> <br><br>书目名称Control Allocation for Spacecraft Under Actuator Faults年度引用<br> http://impactfactor.cn/2024/ii/?ISSN=BK0237226<br><br> <br><br>书目名称Control Allocation for Spacecraft Under Actuator Faults年度引用学科排名<br> http://impactfactor.cn/2024/iir/?ISSN=BK0237226<br><br> <br><br>书目名称Control Allocation for Spacecraft Under Actuator Faults读者反馈<br> http://impactfactor.cn/2024/5y/?ISSN=BK0237226<br><br> <br><br>书目名称Control Allocation for Spacecraft Under Actuator Faults读者反馈学科排名<br> http://impactfactor.cn/2024/5yr/?ISSN=BK0237226<br><br> <br><br>著名 发表于 2025-3-21 21:25:00
Control Allocation for Spacecraft Under Actuator Faults978-981-16-0439-3indemnify 发表于 2025-3-22 03:06:21
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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胰岛素 发表于 2025-3-22 16:46:26
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胰岛素 发表于 2025-3-22 20:02:52
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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 presenceBOOR 发表于 2025-3-23 03:01:22
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领带 发表于 2025-3-23 09:07:16
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