[1]明瑞晨,李吉宽,李 刚,等.无人机纵向着舰下滑轨迹控制技术研究[J].机械与电子,2018,(08):44-46.
　MING Ruichen,LI Jikuan,LI Gang,et al.Research on Longitudinal Automatic Carrier Landing Control for Unmanned Aerial Vehicle[J].Machinery & Electronics,2018,(08):44-46.
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无人机纵向着舰下滑轨迹控制技术研究
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《机械与电子》[ISSN:1001-2257/CN:52-1052/TH]

卷:
期数:
2018年08期
页码:
44-46
栏目:
自动控制与检测
出版日期:
2018-08-24

文章信息/Info

Title:
Research on Longitudinal Automatic Carrier Landing Control for Unmanned Aerial Vehicle
文章编号:
1001-2257(2018)08-0044-03
作者:
明瑞晨1; 李吉宽2; 李 刚2; 刘小雄1
(1.西北工业大学自动化学院, 陕西 西安 710072; 2.空军试飞局, 陕西 西安 710089)
Author(s):
MING Ruichen1; LI Jikuan2; LI Gang2;  LIU Xiaoxiong1
(1.College of Automation, Northwestern Polytechnical University, Xi'an 710072, China; 2.Air Force Flight Test Bureau, Xi'an 710089, China)
关键词:
无人机;  自动着舰;  直接力控制;  轨迹控制
Keywords:
unmanned aerial vehicle;  automatic landing;  direct force control;  trajectory control
分类号:
V249
文献标志码:
A
摘要:
考虑到着舰下滑阶段自动控制的复杂程度,为了在不降低下滑速度的前提下精确控制下滑轨迹,提出一种基于直接力的下滑轨迹控制方法。首先,给出能够产生直接力的无人机控制模型; 接着详细设计了下滑轨迹控制结构; 最后,采用直接升力模态在保持迎角恒定的控制条件下完成了无人机的精确着舰下滑轨迹控制。仿真结果表明,设计的控制方法能够使得无人机很好的完成自动着舰控制。
Abstract:
Considering the complexity of the landing control system of the unmanned aerial vehicle(UAV), this paper applies the direct force control in the design of the landing trajectory control system in order to improve the trajectory control system. Firstly, a UAV model capable of generating direct force was proposed. And then the control structure of landing-guided dynamic tracking was designed. Finally, the direct lift mode was used to control the precise landing trajectory of the drone under the control condition of constant angle of attack. The simulation results show that the control method designed in this paper can make the drone control the automatic landing well.

参考文献/References:

[1] 高丽,吴文海,梅丹,等.侧向自动着舰引导控制L_1自适应设计[J].飞行力学,2016,34(04):41-45.
[2] 郭锁凤. 先进飞行控制系统[M]. 北京:国防工业出版社, 2003.
[3] 杨宝钧, 刘刚, 洪冠新. 雷达信号误差对舰载机全自动着舰控制的影响[J]. 北京航空航天大学学报, 2016, 43(6):1247-1253.
[4] DENISON A.Automated carrier landing of an unmanned combat aerial vehicle using dynamic inversion[R]. Air Force Inst of Tech Wright-patterson Afb Oh School of Engineering and Management, 2007.
[5] BOSKOVIC J, REDDING J. An autonomous carrier landing system for unmannned aerial vehicles[C]∥Aiaa Guidance, Navigation, and Control Conference: American Institute of Aeronautics and Astronautics, 2009: 10-13.
[6] DENHAM J, TAMES W. Advanced controls and displays for precision carrier landings[C]∥54th Aiaa Aerospace Sciences Meeting, 2016: 1770-1784.
[7] LIUMING Y, GANG L, GUANGXIN H. Design and simulation of F/a-18a automatic carrier landing guidance controller[C]∥Aiaa Modeling and Simulation Technologies Conference, 2016: 2514-2525.

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备注/Memo

备注/Memo:
收稿日期:2018-05-17
基金项目:航空科学基金(20150753009); 陕西省飞行控制与仿真技术重点实验室资助
作者简介:明瑞晨(1996-),男,湖北阳新人,硕士研究生,研究方向为飞行控制; 李吉宽(1975-),男,黑龙江宾县人,高级工程师,研究方向为飞行控制; 李 刚(1967-),男,河北昌黎人,高级工程师,研究方向为飞行控制; 刘小雄(1973-),男,陕西周至人,副教授,研究方向为飞行控制、编队控制、旋翼无人机导航控制。
更新日期/Last Update: 2018-08-24