[1]姚克明,刘燕斌,陆宇平,等.火星探测无人机建模与拉起平飞控制[J].南京理工大学学报(自然科学版),2013,37(06):950-954.
 Yao Keming,Liu Yanbin,Lu Yuping,et al.Modeling and pull level flight control for exploration unmanned aerial vehicle on Mars[J].Journal of Nanjing University of Science and Technology,2013,37(06):950-954.
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火星探测无人机建模与拉起平飞控制
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《南京理工大学学报》(自然科学版)[ISSN:1005-9830/CN:32-1397/N]

卷:
37卷
期数:
2013年06期
页码:
950-954
栏目:
出版日期:
2013-12-31

文章信息/Info

Title:
Modeling and pull level flight control for exploration unmanned aerial vehicle on Mars
作者:
姚克明12刘燕斌1陆宇平1郭豫荣3
1.南京航空航天大学 航天学院,江苏 南京 210016;
2.江苏理工学院 电气信息工程学院,江苏 常州 213001;
3.陕西理工学院 电气工程学院,陕西 汉中 723001
Author(s):
Yao Keming12Liu Yanbin1Lu Yuping1Guo Yurong3
1.College of Astronautics,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China;
2.College of Electric Information Engineering,Jiangsu University of Technology,Changzhou 213001,China;
3.College of Electrical Engineering,Shanxi University of Technology,Hanzhong 723001,China
关键词:
火星探测 无人机 拉起平飞控制 模态切换控制方法
Keywords:
Mars exploration unmanned aerial vehicles pull level flight control mode switching control method
分类号:
V271.9
摘要:
为实现火星飞行器动静平衡状态的平滑过渡,满足特定点平飞的巡航要求,该文分析了火星探测无人机的运行过程,建立了火星探测无人机的纵向模型。研究了火星探测无人机拉起和平飞过程的运动特性,归纳了拉起平飞过程的控制难点。采用变控制结构和变控制参数的模态切换控制方法,实现了火星探测无人机的拉起和平飞的有效控制。仿真结果表明该文方法的可行性。
Abstract:
To realize the smooth transition of balance of motion and quiescence of aircrafts and satisfy the cruise requirement of level flight above specific points,the flight processes of a Mars vehicle are analyzed and a longitudinal model of the Mars vehicle is established.The motion characteristics of pull level flight processes of the Mars unmanned aerial vehicle are researched,and the control difficulties of pull level flight processes are summarized.A mode switching control method with variable control structure and control parameters is used to achieve the effective control of pull level flight processes of the Mars unmanned aerial vehicle.The simulation results show that the method proposed here is feasible.

参考文献/References:

[1] Hotchko N.Entry,descent and deployment multi-body simulation for the ARES Mars airplane[R].AIAA-2009-2062,2009.
[2]Brown N,Samuel A,Richard C.Mars exploration airplane:Design,construction,and flight testing of a stability,control,and performance demonstrator[R].AIAA-2007-2723,2007.
[3]Moores J E,Francis,R.A mission control architecture for robotic lunar sample return as field tested in an analogue deployment to the sudbury impact structure[J].Advances in Space Research,2012,50(12):1666-1686.
[4]战培国,钟萍.国外火星探测无人机的研究进展[J].无人机,2011(3):35-37.
Zhan Peiguo,Zhong ping.Foreign research progress of exploration UAV on Mars[J].Unmanned Aerial Vehicle,2011(3):35-37.
[5]Robert D,Henry S,Mark A,et al,Design of the ARES mars airplane and mission architecture[J].Journal of Spacecraftand Rockets,2006,43(5):1026-1034.
[6]Bilimoria K D,Schmidt D K.Integrated development of the equations of motion for elastic hypersonic flight vehicles[J].Journal of Guidance,Control,and Dynamics,1995,18(1):73-81.
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备注/Memo

备注/Memo:
收稿日期:2013-08-16 修回日期:2013-10-22
基金项目:国家自然科学基金(91016017; 61201248); 江苏省自然科学基金(BK20130234); 江苏省高校自然科学基金(13KJD510003)
作者简介:姚克明(1978-),男,博士后,主要研究方向:飞行器控制与自主导航、机器视觉等,E-mail:ykm_1997@163.com。
引文格式:姚克明,刘燕斌,陆宇平,等.火星探测无人机建模与拉起平飞控制[J].南京理工大学学报,2013,37(6):950-954.
投稿网址:http://njlgdxxb.paperonce.org
更新日期/Last Update: 2013-12-31