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战术导弹制导控制系统一体化设计仿真平台
引用本文:杨泗智. 战术导弹制导控制系统一体化设计仿真平台[J]. 火力与指挥控制, 2017, 42(8). DOI: 10.3969/j.issn.1002-0640.2017.08.022
作者姓名:杨泗智
作者单位:西北工业大学航天学院,西安 710072;西北工业集团有限公司,西安 710043
摘    要:对战术导弹的制导控制系统的设计阶段和特点进行了分析研究,对设计流程及所用到的方法进行了研究,在研究的基础上提出了制导控制系统一体化设计仿真分析平台的思路,该平台可用于常规导弹制导控制系统的一体化设计,包括导弹的控制系统设计分析、制导律设计、制导控制系统的数学建模与仿真、半实物仿真分析以及系统性能评估等,具有可扩展性,为战术导弹制导控制系统研究提供模块化手段,加速战术导弹的研制进度。

关 键 词:战术导弹  制导控制  设计  仿真

Research on Integrated Design Simulation Platform of Tactical Missile Guidance and Control System
YANG Si-zhi. Research on Integrated Design Simulation Platform of Tactical Missile Guidance and Control System[J]. Fire Control & Command Control, 2017, 42(8). DOI: 10.3969/j.issn.1002-0640.2017.08.022
Authors:YANG Si-zhi
Abstract:The tactical missile guidance and control system design stage and characteristics are analyzed and studied. The process and the method used for the design are studied. On the basis of research proposed a guidance and control system integration design and simulation platform, the platform can be used for the integrated design of missile guidance and control system,including the design of the control system of the missile analysis,mathematical modeling and Simulation of guidance law design,guidance and control system,semi physical simulation analysis and system performance evaluation,The platform can be extended,for tactical missile guidance and control system research provides modular means and accelerated progress in the development of tactical missile.
Keywords:tactical missile  guided and control  design  simulation
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