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基于可拓学的无人机助推火箭自调整机构的设计与实现
引用本文:刘长亮,丁方正,高飞,殷少锋,鲍传美,李纯军,郭相. 基于可拓学的无人机助推火箭自调整机构的设计与实现[J]. 测控技术, 2012, 31(8): 133-136. DOI: 10.3969/j.issn.1000-8829.2012.08.035
作者姓名:刘长亮  丁方正  高飞  殷少锋  鲍传美  李纯军  郭相
作者单位:1.武汉军械士官学校无人机系机电教研室,湖北武汉,430075;2.武汉军械士官学校训练部,湖北武汉,430075;3.总装备部军械技术研究所,河北石家庄,050000;4.中国人民解放军71521部队64分队,河南新乡,453800
摘    要:对无人机火箭助推起飞问题进行了分析,用形式化的方法明确了研究对象,建立了助推火箭自调整的可拓学模型,通过可拓变换确立了检测量与控制量,并以此为基础设计了可拓控制器,给出了其构建的具体方法并在Matlab中进行了仿真验证.结果表明,基于可拓控制的无人机助推火箭自调整机构具有响应速度快、稳定优秀以及适应能力强等特点.

关 键 词:无人机  助推火箭  可拓分析  自调整  可拓控制

Design and Realization of UAV Solid Rocket Booster Auto-Adjusting System Based on Extenics
LIU Chang-liang , DING Fang-zheng , GAO Fei , YIN Shao-feng , BAO Chuan-mei , LI Chun-jun , GUO Xiang. Design and Realization of UAV Solid Rocket Booster Auto-Adjusting System Based on Extenics[J]. Measurement & Control Technology, 2012, 31(8): 133-136. DOI: 10.3969/j.issn.1000-8829.2012.08.035
Authors:LIU Chang-liang    DING Fang-zheng    GAO Fei    YIN Shao-feng    BAO Chuan-mei    LI Chun-jun    GUO Xiang
Affiliation:1 (1.UAV Mechano-Electrical Teaching Room,Wuhan Ordnance Non-Commissioned Officers Academy,Wuhan 430075,China; 2.Training Department,Wuhan Ordnance Non-commissioned Officers Academy,Wuhan 430075,China; 3.Technical Research Institute of GAD,Shijiazhuang 050000,China; 4.No.64 Element,Unit 71521 of People’s Liberation Army,Xinxiang 453800,China)
Abstract:Through analyzing UAV launching by rocket booster,the object of study is defined by formal method,the extension model of the rocket booster auto-adjusting is established.The detection variable and control variable is derived through the extension transformation,and thus the extension controller is designed.The specific method of construction is given and the simulation in Matlab is carried out.The results show that the UAV rocket booster auto-adjusting system based on extension control characterizes fast response,excellent stability and strong adaptability and others.
Keywords:UAV  booster rocket  extension analysis  auto-adjusting  extension controll
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