某型机进近段高精度相对姿态实时测量技术

李宁宁, 冯一鸣, 陈海洋

李宁宁, 冯一鸣, 陈海洋. 某型机进近段高精度相对姿态实时测量技术[J]. 应用光学, 2020, 41(1): 145-149. DOI: 10.5768/JAO202041.0103003
引用本文: 李宁宁, 冯一鸣, 陈海洋. 某型机进近段高精度相对姿态实时测量技术[J]. 应用光学, 2020, 41(1): 145-149. DOI: 10.5768/JAO202041.0103003
LI Ningning, FENG Yiming, CHEN Haiyang. High-precision relative posture real-time measurement technology for a certain aircraft[J]. Journal of Applied Optics, 2020, 41(1): 145-149. DOI: 10.5768/JAO202041.0103003
Citation: LI Ningning, FENG Yiming, CHEN Haiyang. High-precision relative posture real-time measurement technology for a certain aircraft[J]. Journal of Applied Optics, 2020, 41(1): 145-149. DOI: 10.5768/JAO202041.0103003

某型机进近段高精度相对姿态实时测量技术

基金项目: 海军预研基金项目(3020905060102)
详细信息
    作者简介:

    李宁宁(1989−),女,硕士,工程师,主要从事摄影测量与飞行试验方面的工作。Email:741708356@qq.com

  • 中图分类号: TN967.34

High-precision relative posture real-time measurement technology for a certain aircraft

  • 摘要: 某型机在飞行训练过程中,进近段的二维相对姿态数据对于该型机安全着陆有着至关重要的作用。基于无线网络电台的双向数据传输系统能够实时获取进近段飞机相对理想着陆点的水平、垂直相对位置数据。通过上行链路上传着陆点的姿态数据,下行链路实时下传动动差分后的差分数据,最后在中心控制站进行二次数据处理。该技术获得的进近段二维相对姿态精度达到厘米级,满足飞行训练的需求。同时结合飞机显控数据以及视景图,以多角化动态关联的方式将实时获取的姿态数据等呈现给指挥员,更好地辅助指挥员进行着陆指挥工作。
    Abstract: During the flight training of one machine, the two-dimensional relative attitude data of the approach segment plays a crucial role in the safe landing of the aircraft. The two-way data transmission system based on the wireless network radio station can obtain the horizontal and vertical relative position data of the approaching aircraft relative to the ideal landing point in real time. The attitude data of the landing point is uploaded through the uplink, the differential data after the dynamic difference is driven in the downlink, and finally the secondary data processing is performed at the central control station. The two-dimensional relative attitude accuracy of the approach segment obtained by the technology reaches the centimeter level, which satisfies the requirements of flight training. At the same time, combined with the aircraft’s display control data and the visual map, the real-time acquired attitude data is presented to the commander in a multi-angled dynamic association manner, and the assistant commander is better assisted in the landing command work.
  • 图  1   硬件平台测量系统

    Figure  1.   Hardware platform measurement system

    图  2   实时差分与事后差分对比(横向时间/s,纵向距离/m)

    Figure  2.   Real-time differential and post-mortem differential comparison

    图  3   辅助指挥系统平面显示

    Figure  3.   Auxiliary command system flat display

  • [1] 杜红兵, 李珍香. 进近着陆运输飞行事故原因及预防对策研究[J]. 中国安全科学学报,2006,16(6):118-122. doi: 10.3969/j.issn.1003-3033.2006.06.022

    DU Hongbing, LI Zhenxiang. Study on causes and preventive countermeasures of approaching landing flight accidents[J]. Chinese Journal of Safety Science,2006,16(6):118-122. doi: 10.3969/j.issn.1003-3033.2006.06.022

    [2] 李晓明. 进近着陆阶段飞行安全的综合分析与建模[D]. 南京: 南京航天航空大学, 2014: 1-49.

    LI Xiaoming. Comprehensive analysis and modeling of flight safety during approach landing[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2014: 1-49.

    [3] 张涛, 项恒. 基于模糊正态分布的进近段风险评价[J]. 沈阳理工大学学报,2017(2):107-110. doi: 10.3969/j.issn.1003-1251.2017.02.021

    ZHANG Tao, XIANG Heng. Risk assessment of approach segment based on fuzzy normal distribution[J]. Journal of Shenyang Ligong University,2017(2):107-110. doi: 10.3969/j.issn.1003-1251.2017.02.021

    [4] 邹复民, 蒋新华. 多跳Mesh网络无线骨干回传链路性能研究与优化[J]. 科学技术与工程,2008,8(13):3678-3681. doi: 10.3969/j.issn.1671-1815.2008.13.067

    ZOU Fumin, JIANG Xinhua. Research and optimization of wireless backhaul link performance of multi-hop mesh network[J]. Science Technology and Engineering,2008,8(13):3678-3681. doi: 10.3969/j.issn.1671-1815.2008.13.067

    [5]

    HUANG Renjun, XIAO Zongkai. A secure and reliable routing protocal for wireless mesh networks.[J]. J. Shanghai Jiaotong Univ. (Sci.),2014,19(4):466-475. doi: 10.1007/s12204-014-1526-2

    [6] 翟智, 王跃科, 陈建云. 星间链路天线相对姿态的地面模拟[J]. 宇航计测技术,2010,30(6):39-43. doi: 10.3969/j.issn.1000-7202.2010.06.009

    ZHAI Zhi, WANG Yueke, CHEN Jianyun. Ground simulation of relative position of inter-satellite link antenna[J]. Journal of Astronautic Metrology,2010,30(6):39-43. doi: 10.3969/j.issn.1000-7202.2010.06.009

    [7] 郑庆晖. 基于GPS的航天器姿态相对姿态确定研究[D]. 长沙: 国防科学技术大学, 2003(2): 1-153.

    ZHENG Qinghui. Research on attitude and relative attitude determination of spacecraft based on GPS[D]. Changsha: National University of Defense Technology, 2003(2): 1-153.

    [8] 刘万科, 楼益栋, 张小红. 单频伪距差分模型用于动动目标监控的研究与实现[J]. 测绘信息与工程,2004,29(2):36-38. doi: 10.3969/j.issn.1007-3817.2004.02.015

    LIU Wanke, LOU Yidong, ZHANG Xiaohong. Research and implementation of single frequency pseudo range differential model for moving target monitoring[J]. Surveying and Mapping Information and Engineering,2004,29(2):36-38. doi: 10.3969/j.issn.1007-3817.2004.02.015

    [9] 汪捷, 徐冠楠. 基于GNSS动差分相对定位方法的研究与探讨[J]. 现代导航,2015(3):250-256.

    WANG Jie, XU Guannan. Move difference relative positioning methond based on GNSS[J]. Modern Navigation,2015(3):250-256.

    [10] 赵亮, 叶世榕, 陈德忠, 等. 组合观测值确定L1&L2的模糊度的探讨[J]. 测绘地理信息,2013(4):36-38.

    ZHAO Liang, YE Shizhen, CHEN Dezhong, et al. Discussion on the determination of the ambiguity of L1&L2 by combined observations[J]. Surveying and Mapping Geographic Information,2013(4):36-38.

    [11] 韦庆洲, 罗兆文, 朱昱, 等. 基于GPS的飞机姿态实时测量实现及误差分析[J]. 测绘科学,2010(4):20-22.

    WEI Qingzhou, LUO Zhaowen, ZHU Yu, et al. Real-time measurement and error analysis of aircraft attitude based on GPS[J]. Science of Surveying and Mapping,2010(4):20-22.

    [12] 高珊, 韩艳铧. 一种基于机器视觉的航天器交会对接相对位置和姿态确定算法研究[J]. 航天控制,2011,29(1):31-36.

    GAO Shan, HAN Yanhua. A machine vision based algorithm for the determination of relative position and attitude of spacecraft church docking[J]. Space Control,2011,29(1):31-36.

    [13] 王锋, 李彬, 张德贤, 等. 飞行目标姿态测量中测量站点布设方案研究[J]. 光子学报,2007,36(S1):174-176.

    WANG Feng, LI Bin, ZHANG Dexian, et al. Research on measurement site deployment scheme in flight target attitude measurement[J]. Acta Photonica Sinica,2007,36(S1):174-176.

    [14] 赵彩英, 张兴国. 基于多源信息融合的空中运动目标定位技术[J]. 测控技术,2012,31(6):26-28. doi: 10.3969/j.issn.1000-8829.2012.06.007

    ZHAO Caiying, ZHANG Xingguo. Air moving target localization technology based on multi-source information fusion[J]. Measurement and Control Technology,2012,31(6):26-28. doi: 10.3969/j.issn.1000-8829.2012.06.007

    [15] 马令坤. 进近着陆指挥辅助系统-图像处理模块的实现[D]. 西安: 西北工业大学, 2003: 1-71.

    MA Lingkun. Approach landing command assistant system-image processing module implementation[D]. Xi’an: Northwestern Polytechnical University, 2003: 1-71.

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出版历程
  • 收稿日期:  2019-07-24
  • 修回日期:  2019-11-19
  • 网络出版日期:  2020-03-30
  • 刊出日期:  2019-12-31

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