Maneuver Detection and Track for HBG Aircraft Based on IMM Algorithm

摘要：

　　The research works on maneuver detection and tracking technology for the hypersonic boost-glide (HBG) aircraft.Firstly,its motion models are presented by the earlier research.Then,a maneuver detection method is proposed applying interactive multi-mode (IMM) algorithm based on the switch time of model probability for the hypersonic target.Finally the effective and continuous tracking is realized for the HBG aircraft based on space-based platform,employing interactive multi- mode with unscented Kalman filter (IMM-UKF) algorithm for nonlinear filtering.The results show that the models are accurate and the IMM-UKF algorithm is valid.

关键词： hypersonic boost-glide aircraft motion model nonlinear filtering maneuver detection tracking

作者: Shenda Xu Peng You Shaowei Yong

作者单位: College of Electronic Science and Engineering, National University of Defense Technology, Changsha 410073,Hunan, China

会议类型: 国际会议

会议名称: 2016 Sixth International Conference on Instrumentation and Measurement,Computer,Communication and Control (IMCCC2016)(第六届仪器测量、计算机通信与控制国际会议)

会议地点: 哈尔滨

会议语种:英文

页码: 384-388

在线出版日期: 2016-07-21（万方平台首次上网日期，不代表论文的发表时间）