期刊文献+

Three-dimensional analysis of relationship between relative orientation and motion modes

Three-dimensional analysis of relationship between relative orientation and motion modes
原文传递
导出
摘要 Target motion modes have a close relationship with the relative orientation of missile-totarget in three-dimensional highly maneuvering target interception. From the perspective of relationship between the sensor coordinate system and the target body coordinate system, a basic model of sensor is stated and the definition of relative angular velocity between the two coordinate systems is introduced firstly. Then, the three-dimensional analytic expressions of relative angular velocity for different motion modes are derived and simplified by analyzing the influences of target centroid motion, rotation around centroid and relative motion. Finally, the relationships of the relative angular velocity directions and values with motion modes are discussed. Simulation results validate the rationality of the theoretical analysis. It is demonstrated that there are significant differences of the relative orientation in different motion modes which include luxuriant information about motion modes. The conclusions are significant for the research of motion mode identification,maneuver detection, maneuvering target tracking and interception using target signatures. Target motion modes have a close relationship with the relative orientation of missile-totarget in three-dimensional highly maneuvering target interception. From the perspective of relationship between the sensor coordinate system and the target body coordinate system, a basic model of sensor is stated and the definition of relative angular velocity between the two coordinate systems is introduced firstly. Then, the three-dimensional analytic expressions of relative angular velocity for different motion modes are derived and simplified by analyzing the influences of target centroid motion, rotation around centroid and relative motion. Finally, the relationships of the relative angular velocity directions and values with motion modes are discussed. Simulation results validate the rationality of the theoretical analysis. It is demonstrated that there are significant differences of the relative orientation in different motion modes which include luxuriant information about motion modes. The conclusions are significant for the research of motion mode identification,maneuver detection, maneuvering target tracking and interception using target signatures.
出处 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2014年第6期1495-1504,共10页 中国航空学报(英文版)
基金 supported by the Specialized Research Fund for the Doctoral Program of China Higher Education (No. 20134307110012) the National Natural Science Foundation of China (No. 61101186)
关键词 Attitude analysis Coordinate system Motion mode Relative angular velocity Sensor Terminal guidance Attitude analysis Coordinate system Motion mode Relative angular velocity Sensor Terminal guidance
  • 相关文献

参考文献18

  • 1Fan HQ, Zhu YL, Fu Q. Impact of mode decision delay on estimation error for maneuvering target interception. IEEE Trans Aerosp Electron Syst 2011;47(1):702-11.
  • 2Shinar J, Shima T. Game theoretical interceptor guidance law for ballistic missile defense. Proceedings of the 35th conference on decision and control; 1996 December 11-13; Kobe, Japan; 1996. p. 2780-85.
  • 3Shinar J, Shima T. Nonorthodox guidance law development approach for intercepting maneuvering targets. J Guidance Control Dyn 2002;25(4):658-66.
  • 4Shinar J, Oshman Y. Optimal integration of estimation and guidance for interceptors, 0704-0188. Haifa: Israel Institute of Technology; 2005.
  • 5Shinar J, Glizer VY. New approach to improve the accuracy in delayed information pursuit-evasion games. Ann Int Soc Dyn Games 2006;8:65-103.
  • 6Oshman Y, Arad D. Enhanced air-to-air missile tracking using target orientation observations. J Guidance Control Dyn 2004;27(4):595-606.
  • 7Shima T, Oshman Y, Shinar J. Efficient multiple model adaptive estimation in ballistic missile interception scenarios. J Guidance Control Dyn 2002;25(4):667-75.
  • 8Fan HQ. Technology on maneuvering target motion mode identification in active homing guidance dissertation. Changsha: National University of Defense Technology; 2008.
  • 9Zhu YL, Fan HQ, Fu Q. Target turning maneuver detection using high resolution Doppler profile. IEEE Trans Aerosp Electron Syst 2012;48(1 ):762-79.
  • 10Zhu YL, Fan HQ, Lu ZQ. A novel maneuver detector based on back propagation neural network. Signal Process 2011;91(4): 1054-9.

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部