高超声速滑翔飞行器长期轨迹预测问题探讨
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  • 英文篇名:Discussion on Long-Term Trajectory Prediction of Hypersonic Gliding Reentry Vehicle
  • 作者:张凯 ; 熊家军
  • 英文作者:Zhang Kai;Xiong Jiajun;Department of Graduation Management,Air Force Early Warning Academy;Air Force Early Warning Academy;
  • 关键词:高超声速飞行器 ; 再入滑翔 ; 轨迹预测 ; 状态估计 ; 意图推断
  • 英文关键词:hypersonic vehicle;;reentry glide;;trajectory prediction;;state estimation;;intent inference
  • 中文刊名:ZSDD
  • 英文刊名:Tactical Missile Technology
  • 机构:空军预警学院研究生管理大队;空军预警学院;
  • 出版日期:2018-07-15
  • 出版单位:战术导弹技术
  • 年:2018
  • 期:No.190
  • 基金:国家863计划项目(No.2015AA8017032P);; 全军军事类研究生资助课题(2016JY312)
  • 语种:中文;
  • 页:ZSDD201804003
  • 页数:6
  • CN:04
  • ISSN:11-1771/TJ
  • 分类号:19-23+43
摘要
为给高超声速滑翔飞行器态势与威胁评估、反导拦截提供先验知识,探讨基于状态估计和意图推断的长期轨迹预测方法。对飞行器的控制特性进行阐述,分析了长期轨迹预测的可行性。针对飞行器机动不确定的问题,综合考虑飞行器当前状态和作战意图,阐述了长期轨迹预测的基本思想。最后,分别从预测模型构建、预测误差修正、制导规律辨识和意图信息推断四个方面讨论了飞行器长期轨迹预测的关键技术。
        In order to provide a priori knowledge for situation and threat assessment and interception of hypersonic gliding reentry vehicle,a long-term trajectory prediction method based on state estimation and intention inference is discussed. Firstly,the vehicle's control characteristics are described to analyze the feasibility of long-term trajectory prediction. In view of target maneuver,the idea of long-term trajectory prediction considering the current state and combat intent is proposed. Then some key technologies of long-term trajectory prediction are discussed respectively from aspects of prediction modeling,prediction error correction,control law identification and intent information inference.
引文
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