发布求助
文献互助 智能选刊 最新文献

Control Allocation for Spacecraft Under Actuator Faults最新文献

筛选
英文 中文
Finite-Time Fault-Tolerant Spacecraft Attitude Control with Torque Saturation 考虑转矩饱和的有限时间容错航天器姿态控制
Control Allocation for Spacecraft Under Actuator Faults Pub Date : 2017-08-02 DOI: 10.2514/1.G002191
Q. Hu, Xiao Tan, M. Akella
{"title":"Finite-Time Fault-Tolerant Spacecraft Attitude Control with Torque Saturation","authors":"Q. Hu, Xiao Tan, M. Akella","doi":"10.2514/1.G002191","DOIUrl":"https://doi.org/10.2514/1.G002191","url":null,"abstract":"A smooth attitude-stabilizing controller is proposed for rigid spacecraft actuated by thrusters that achieves finite-time stability in the presence of external disturbance, input saturation, and in...","PeriodicalId":440591,"journal":{"name":"Control Allocation for Spacecraft Under Actuator Faults","volume":"105 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2017-08-02","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"131058237","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 43
Nonlinear Proportional-Derivative Control Incorporating Closed-Loop Control Allocation for Spacecraft 基于闭环控制分配的航天器非线性比例导数控制
Control Allocation for Spacecraft Under Actuator Faults Pub Date : 2014-04-25 DOI: 10.2514/1.61815
Q. Hu, Bo Li, Youmin Zhang
{"title":"Nonlinear Proportional-Derivative Control Incorporating Closed-Loop Control Allocation for Spacecraft","authors":"Q. Hu, Bo Li, Youmin Zhang","doi":"10.2514/1.61815","DOIUrl":"https://doi.org/10.2514/1.61815","url":null,"abstract":"A novel saturated proportional-derivative control law incorporated with closed-loop control allocation is proposed for spacecraft attitude stabilization in this paper. More specifically, a saturated proportional-derivative-based baseline nonlinear controller is designed to guarantee the globally asymptotic stability under control input/signal constraints. Then, a closed-loop constrained optimal control allocation scheme is employed to distribute the moments synthesized by the baseline controller over the redundant actuators in the presence of constraints due to actuator amplitude and rate constraints. The optimal control solution is to be found by penalizing the control allocation errors and rates using optimal quadratic programming algorithms. A significant feature of this work is that the asymptotic stability with the closed-loop control allocation is guaranteed theoretically. Simulation results are presented to illustrate the performance of the proposed scheme.","PeriodicalId":440591,"journal":{"name":"Control Allocation for Spacecraft Under Actuator Faults","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2014-04-25","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"130753020","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 34
Closed-Loop Based Control Allocation for Spacecraft Attitude Stabilization with Actuator Faults 带有执行器故障的航天器姿态稳定闭环控制分配
Control Allocation for Spacecraft Under Actuator Faults Pub Date : 1900-01-01 DOI: 10.1007/978-981-16-0439-3_9
Q. Hu, Bo Li, B. Xiao, Youmin Zhang
{"title":"Closed-Loop Based Control Allocation for Spacecraft Attitude Stabilization with Actuator Faults","authors":"Q. Hu, Bo Li, B. Xiao, Youmin Zhang","doi":"10.1007/978-981-16-0439-3_9","DOIUrl":"https://doi.org/10.1007/978-981-16-0439-3_9","url":null,"abstract":"","PeriodicalId":440591,"journal":{"name":"Control Allocation for Spacecraft Under Actuator Faults","volume":"41 4","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"133135940","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 1
Conclusions 结论
Control Allocation for Spacecraft Under Actuator Faults Pub Date : 1900-01-01 DOI: 10.1007/978-981-16-0439-3_10
Qing-bin Hu, Bo Li, Bing Xiao, Youmin Zhang
{"title":"Conclusions","authors":"Qing-bin Hu, Bo Li, Bing Xiao, Youmin Zhang","doi":"10.1007/978-981-16-0439-3_10","DOIUrl":"https://doi.org/10.1007/978-981-16-0439-3_10","url":null,"abstract":"","PeriodicalId":440591,"journal":{"name":"Control Allocation for Spacecraft Under Actuator Faults","volume":"1 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"124683380","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
0
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整，为了账户安全，请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
现在去查看 取消
×
提示
确定
请完成安全验证×
相关产品
×
本文献相关产品
联系我们：info@booksci.cn Book学术提供免费学术资源搜索服务，方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号：481959085
Book学术官方微信