Three-Dimensional Discrete Observability Analysis for Air-to-Air Missile Target Tracking

被引：0
|
作者：
Liu F. [1 ,2 ]
Ren Z. [1 ]
Liang Y. [1 ]
机构：
[1] School of Autonomous Science and Electrical Engineering, Beihang University, Beijing
[2] Department of General Aviation, Civil Aviation Management Institute of China, Beijing
来源：
Ren, Zhang (renzhang@buaa.edu.cn) | 1600年 / Beijing Institute of Technology卷 / 26期
基金：
中国国家自然科学基金;
关键词：
3D discrete system; Air-to-air missile (AAM); Observability analysis; Target tracking;
D O I：
10.15918/j.jbit1004-0579.201726.0415
中图分类号：
学科分类号：
摘要：
The interception information of infrared (IR)-guided air-to-air missiles (AAM) is mainly estimated only using the basic bearing measurements. In order to intercept highly maneuverable targets, it is essential to study the system observability to improve the target tracking system performance. The uniqueness of this paper is that the observability analysis is derived based on a discrete three-dimensional(3D) system model. During the maneuvering scenario, the system is approximated by a segment-by-segment system. The relationship between missile-target motion and observability is given by direct and dual approaches. Meanwhile sufficient observability conditions are derived. Moreover, a numerical simulation is conducted and an alternate method is provided to reinforce the proposed observability analysis results. © 2017 Editorial Department of Journal of Beijing Institute of Technology.
引用
收藏
页码：548 / 556
页数：8
相关论文
共 50 条
  • [41] Flush air data sensing system design for air breathing air-to-air missile
    Chen G.
    Liu W.
    Dou X.
    Zhou W.
    Dou G.
    Chen, Guangqiang (guangqiangchen@sina.com), 1600, Chinese Academy of Sciences (46): : 1193 - 1206
  • [42] Raytheon and MBDA battle for air-to-air missile market share
    不详
    AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2007, 79 (03): : 296 - 296
  • [43] EIGENSTRUCTURE ASSIGNMENT FOR THE EXTENDED MEDIUM RANGE AIR-TO-AIR MISSILE
    SOBEL, K
    CLOUTIER, JR
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1992, 15 (02) : 529 - 531
  • [44] Separation Dynamics of Air-to-Air Missile and Validation with Flight Data
    Anandhanarayanan, K.
    Raj, Ankit
    Shah, Vaibhav
    Krishnamurthy, R.
    Chakraborty, Debasis
    DEFENCE SCIENCE JOURNAL, 2018, 68 (01) : 5 - 11
  • [45] CRITICAL AERODYNAMIC TECHNOLOGY ISSUES IN AIR-TO-AIR MISSILE DESIGN
    GIRAGOSIAN, PA
    ASTRONAUTICS & AERONAUTICS, 1979, 17 (7-8): : B41 - B41
  • [46] Coefficient diagram robust control design for air-to-air missile
    Zhao, Jinlei
    Cao, Junyi
    Ma, Chengbin
    Zhou, Shengxi
    Cao, Binggang
    Hsi-An Chiao Tung Ta Hsueh/Journal of Xi'an Jiaotong University, 2013, 47 (11): : 70 - 75
  • [47] A Near Optimal Midcourse Guidance Law for Air-to-Air Missile
    Qiao Qingqing
    Chen Wanchun
    INDUSTRIAL INSTRUMENTATION AND CONTROL SYSTEMS II, PTS 1-3, 2013, 336-338 : 833 - 838
  • [48] AIR-TO-AIR MISSILE AIRFRAME CAPTIVE FLIGHT VIBROACOUSTIC ENVIRONMENT
    POYNOR, SP
    JOURNAL OF THE IES, 1990, 33 (04): : 44 - 52
  • [49] Research on Fast Calculation Technology of Air-to-Air Missile Impact Area
    Zhang, Yijie
    Wu, Yong
    Zhang, Yi
    Yue, Longfei
    PROCEEDINGS OF THE IEEE 2019 9TH INTERNATIONAL CONFERENCE ON CYBERNETICS AND INTELLIGENT SYSTEMS (CIS) ROBOTICS, AUTOMATION AND MECHATRONICS (RAM) (CIS & RAM 2019), 2019, : 245 - 250
  • [50] Multidisciplinary integrated design optimization for an airbreathing air-to-air missile shape
    Wang R.
    Zhang H.
    Wang G.
    Chen G.
    Bai P.
    Zhang Z.
    Li X.
    Fu J.
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2016, 37 (01): : 207 - 215
12345