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一种适用于复合制导的中末制导弹道交接班方法
引用本文:刘钧圣,陈士超,陈韵,段辰璐,刘明. 一种适用于复合制导的中末制导弹道交接班方法[J]. 战术导弹技术, 2020, 0(2): 51-56,92
作者姓名:刘钧圣  陈士超  陈韵  段辰璐  刘明
作者单位:西北工业大学航天学院;中国兵器工业第203研究所第一总体部;陕西师范大学计算机科学学院
基金项目:国家自然科学基金(61701289);陕西省自然科学基金(2018JQ6083,2018JQ6087);陕西省高校科协青年人才托举计划(20190106)。
摘    要:导弹武器系统的发展趋势是由单一制导模式向复合制导过渡,而中末制导的可靠交接班是复合制导的关键步骤。针对复合制导中的中末制导弹道交接班问题,在分析中末制导弹道平滑过渡约束条件的基础上,提出了一种简单有效的线性中末制导交接班算子,详细计算了平滑算子的加权系数。通过直升机载空地导弹的中末制导弹道交接班的仿真试验,验证所提方法的可行性。试验结果表明,在较小中末制导律差异条件下,所提算子可实现弹道的平滑过渡和良好衔接。

关 键 词:复合制导  中末制导交接班  平滑算子  导弹  弹道

A Midcourse and Terminal Trajectory Handover Method Suitable for Composite Guidance Missiles
Liu Junsheng,Chen Shichao,Chen Yun,Duan Chenlu,Liu Ming. A Midcourse and Terminal Trajectory Handover Method Suitable for Composite Guidance Missiles[J]. Tactical Missile Technology, 2020, 0(2): 51-56,92
Authors:Liu Junsheng  Chen Shichao  Chen Yun  Duan Chenlu  Liu Ming
Affiliation:(School of Astronautics,Northwestern Polytechnical University,Xi’an 710072,China;No.1 General Department,No.203 Research Institute of China Ordnance Industries,Xi’an 710065,China;School of Computer Science,Shanxi Normal University,Xi’an 710119,China)
Abstract:Transition from single guidance mode to compound guidance is the development trend of missile weapon system,and the key point of the process is to realize trajectory transition between midcourse and terminal guidance robustly. Focusing on the problem of midcourse and terminal guidance transition,based on the analysis of the constraints of trajectory smooth transition,a simple but effective method is proposed to realize smooth transition by using a linear operator. The weighted coefficients are calculated and analyzed in detail. The effectiveness of the proposed method is tested on the simulated data of helicopter-borne air-to-ground missiles. And the experimental results show that the proposed linear operator is capable of realizing smooth transition and good connection under the condition of small difference between midcourse and terminal guidance.
Keywords:composite guidance  midcourse and terminal guidance handover  smooth factor  missile  trajectory
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