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基于空中非合作目标的多目标探测技术

Multi-target Detection Technology Based on Air Non-cooperative Targets
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摘要 开展机载雷达多目标探测能力飞行试验需要的配试目标机数量多,而在实际试验过程中由于配试资源有限,仅使用有限数量的合作目标机作为配试资源,对其能力的验证不充分。笔者针对机载雷达多目标探测试飞配试目标机数量不足的问题,提出了使用空中非合作目标作为配试目标的试验方法,并应用在实际试飞中,提高了试飞效率。 Airborne radar multi-target detection ability flight test need to match a lot of targets, and have to use only a limited number of cooperation targets as flight test resource. The author in view- of the airborne radar multi-target detection flight test with the problem of insufficient number target, proposed to use air non-cooperative target as a worthy goal of flight test, and applied in the actual test, improved the test efficiency.
作者 韩春永 周慧楠 Han Chunyong;Zhou Huinan(Chinese Flight Test Establishment,Xi'an Shaanxi 710089,China)
出处 《信息与电脑》 2018年第12期36-38,51,共4页 Information & Computer
关键词 多目标探测 非合作目标 飞行试验 muhi-target detection non-cooperative target flight test
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  • 1张庆君,胡修林,叶斌,钟山.基于双目视觉的航天器间相对位置和姿态的测量方法[J].宇航学报,2008,29(1):156-161. 被引量:44
  • 2陆彦.航空火力控制技术[M].北京:国防工业出版社,1994..
  • 3[6] 陈士橹,吕学富. 导弹飞行力学 [M]. 西安: 西北工业大学出版社,1983.
  • 4Park C, Ferguson P, Pohlman N, et al. Decentralized relative navigation for formation flying spacecraft using augmented CDGPS [ C ]. Institute of Navigation GPS Conference, Salt Lake City, Utah, Sept. 1 -12, 2001.
  • 5Son-Goo K, John L C, Yang C, et al. Kalman filtering for relative spacecraft attitude and position estimation [ J]. Journal of Guidance Control and Dynamics, 2007, 30( 1 ) : 133 - 143.
  • 6Philip N K, Ananthasayanam M R. Relative position and attitude estimation and control schemes for the final phase of an autonomous docking mission of spacecraft [ J ]. Acta Astronautica, 2003. 52:511 -522.
  • 7Ho C J, Mcdlamroch N H. Automatic spacecraft docking using computer vlsion-based guidance and control techniques[ J].Journal of Guidance, Control and Dynamics, 1993, 16(2) : 281 -288.
  • 8Farrenkopf R L. Analytic steady-state accuracy solution for two common spacecraft attitude estimators [ J ]. Journal of Guidance and Control, 1978, 1 (4):282-284.
  • 9Xing G Q, Parvez S A. Nonlinear attitude state tracking control for spacecraft[J]. Journal of Guidance, Control and Dynamics, 2001, 24(3): 624-626.
  • 10靳永强,刘向东,侯朝桢.基于UKF的无陀螺姿态确定[J].航天控制,2007,25(4):31-35. 被引量:8

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