中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
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浏览/检索结果: 共8条,第1-8条 帮助

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Flight verification of cooling self-sustaining high-temperature superconducting motor 期刊论文  OAI收割
SUPERCONDUCTOR SCIENCE & TECHNOLOGY, 2024, 卷号: 37
作者:  
Zheng, Jinxing;  Sun, Jinxin;  Liu, Fei;  Liu, Xufeng;  Peng, Junyi
  |  收藏  |  浏览/下载:11/0  |  提交时间:2024/11/20
Unmanned Aerial Vehicle Formation Inspired by Bird Flocking and Foraging Behavior 期刊论文  OAI收割
International Journal of Automation and Computing, 2018, 卷号: 15, 期号: 4, 页码: 402-416
作者:  
Tian-Jie Zhang
  |  收藏  |  浏览/下载:68/0  |  提交时间:2021/02/23
Control techniques of tilt rotor unmanned aerial vehicle systems: A review 期刊论文  OAI收割
Chinese Journal of Aeronautics, 2017, 卷号: 30, 期号: 1, 页码: 135-148
作者:  
Liu Z(刘重);  He YQ(何玉庆);  Yang LY(杨丽英);  Han JD(韩建达)
收藏  |  浏览/下载:24/0  |  提交时间:2017/02/05
Dynamics modelling and predictive control for 6-DOF rotorcraft aerial manipulator system 期刊论文  OAI收割
International Journal of Modelling, Identification and Control, 2016, 卷号: 26, 期号: 3, 页码: 227-237
作者:  
Song DL(宋大雷);  Qi JT(齐俊桐)
  |  收藏  |  浏览/下载:29/0  |  提交时间:2017/12/11
System of systems oriented flight vehicle conceptual design: Perspectives and progresses 期刊论文  OAI收割
Chinese Journal of Aeronautics, 2015, 卷号: 28, 期号: 3, 页码: 617-635
作者:  
Liu Hu;  Tian Yongliang;  Gao Yuan;  Bai Jinpeng;  Zheng Jiangan
  |  收藏  |  浏览/下载:22/0  |  提交时间:2021/02/02
高超声速飞行器鲁棒自适应飞行控制方法研究 学位论文  OAI收割
工学博士, 中国科学院自动化研究所: 中国科学院大学, 2014
作者:  
杨芳
收藏  |  浏览/下载:124/0  |  提交时间:2015/09/02
Reentry guidance based on feedback linearization (EI CONFERENCE) 会议论文  OAI收割
2011 International Conference on Electronics, Communications and Control, ICECC 2011, September 9, 2011 - September 11, 2011, Ningbo, China
Li D.-W.
收藏  |  浏览/下载:31/0  |  提交时间:2013/03/25
This paper presents a new reentry guidance algorithm for RLV (Reusable Launching Vehicle). The algorithm consists of two integrated components: trajectory planning algorithm and tracking algorithm. The most striking feature of algorithm here lies in that both planning and tracking are executed directly in height-velocity space  which is different from the methodology of configuration of drag in traditional shuttle guidance. In the session of trajectory planning  all trajectory constraints can be expressed with upper bound and lower bound in height-velocity space  then a linear interpolation is carried to search the nominal trajectory satisfying the requirement of downrange and target constraints. Then the tracking algorithm uses feedback linearization method to track this nominal profile and meet all constraints. Another typical feature of this algorithm is the strategy of downrange extension using FPA (flight path angle) controller to fulfill the requirement of large downrange. Proper combination of planning-tracking algorithm and FPA controller can bring great flexibility and adaptability to reentry guidance. The algorithm is proved to be robust enough to accommodate the model error and noises in the dynamics. 2011 IEEE.  
多操纵面无人机控制分配技术研究 学位论文  OAI收割
工学博士, 中国科学院自动化研究所: 中国科学院研究生院, 2010
作者:  
王会东
收藏  |  浏览/下载:184/0  |  提交时间:2015/09/02