A Regression Application for Conversion of Static Missile Signature to Dynamic Missile Signature

被引:0
|
作者
Soybas, Zafer [1 ]
Sahingil, Mehmet Cihan [1 ]
机构
[1] TUBITAK BILGEM ILTAREN, Ankara, Turkey
来源
2022 30TH SIGNAL PROCESSING AND COMMUNICATIONS APPLICATIONS CONFERENCE, SIU | 2022年
关键词
UV Sensor; Missile UV Signature; Regression; Missile; Machine Learning;
D O I
10.1109/SIU55565.2022.9864996
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
The UV (ultraviolet) based sensors identify the missiles with an algorithm that it runs by visually detecting the UV signature of the hot missile exhaust and extracting the threat features from these images. These features can be used in algorithm improvements by measuring with UV sensors placed on the ground projection of the missile flight route in live missile tests where missiles are fired to a hot target. However, live missile tests are difficult and costly processes. In addition, it is not possible to take measurements with UV sensors from every angle and range required in these tests. For these reasons, it is important to convert the UV signatures obtained as a result of firing the stationary missile engine in a suitable environment into missile signatures approaching towards the UV sensors. Within the scope of this study, the regression studies aimed to convert the UV signatures (static missile signature) taken from the fixed engine burning tests of various missiles into the UV signatures (dynamic missile signature) of the missiles approaching towards the UV sensors are summarized.
引用
收藏
页数:4
相关论文
共 50 条
  • [21] DYNAMIC STABILITY OF A MISSILE IN ROLLING FLIGHT
    BOLZ, RE
    JOURNAL OF THE AERONAUTICAL SCIENCES, 1952, 19 (06): : 395 - 403
  • [22] DYNAMIC ASPECTS OF ARMY MISSILE SYSTEMS
    GREEN, PL
    JOURNAL OF ENVIRONMENTAL SCIENCES, 1985, 28 (05): : 40 - 44
  • [23] Structural dynamic modelling and testing of a missile
    Yildirim, E. G. Yalcin
    PROCEEDINGS OF INTERNATIONAL CONFERENCE ON NOISE AND VIBRATION ENGINEERING (ISMA2020) / INTERNATIONAL CONFERENCE ON UNCERTAINTY IN STRUCTURAL DYNAMICS (USD2020), 2020, : 1081 - 1085
  • [24] CONVERSION OF A BARGE FOR VERTICAL LAUNCH MISSILE TRIALS
    不详
    NAVAL ARCHITECT, 1985, (MAY): : E239 - E239
  • [25] Dynamic Characteristics Analysis of Elastic Missile
    Xu Zhaoqing
    Pei Hailong
    2016 IEEE CHINESE GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC), 2016, : 98 - 102
  • [26] Dynamic stability of a rolling flexible missile
    GLASSON AR
    1970, MC6 (01): : 15 - 18
  • [27] APPLICATION OF COMPOSITES TO MISSILE STRUCTURES - A REVIEW
    BAILIE, JA
    SAMPE QUARTERLY-SOCIETY FOR THE ADVANCEMENT OF MATERIAL AND PROCESS ENGINEERING, 1981, 12 (02): : 1 - 8
  • [28] Application of QFT for missile flight control
    Zhang, J.-W. (hellozjw@bit.edu.cn), 1600, Beijing Institute of Technology (33):
  • [29] Dynamic robust recursive control design and its application to a nonlinear missile autopilot
    Hull, RA
    Qu, ZH
    PROCEEDINGS OF THE 1997 AMERICAN CONTROL CONFERENCE, VOLS 1-6, 1997, : 833 - 837
  • [30] Dynamic group signature with forward security and its application
    Zhou, Xuanwu
    Yang, Xiaoyuan
    Wei, Ping
    Hu, Yupu
    SIXTH INTERNATIONAL CONFERENCE ON GRID AND COOPERATIVE COMPUTING, PROCEEDINGS, 2007, : 473 - +