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飞航导弹三通道半实物全弹道仿真的静态和动态调试
引用本文:顾文锦.飞航导弹三通道半实物全弹道仿真的静态和动态调试[J].战术导弹技术,1991(1):23-28.
作者姓名:顾文锦
作者单位:海军航空工程学院
摘    要:本文以我院已研制成功的“海军导弹武器系统仿真工程”为背景,着重介绍了其中三通道半实物飞行仿真子系统的组成、功用及静态和动态调试,为进行战术飞航导弹的同类仿真研究提供了一定的经验。

关 键 词:导弹  仿真  静态动态调试

STATIC AND DYNAMIC ADJUSTMENT OF SIX-DEGREE-OF-FREEDOM SIMULATION SYSTEM FOR CRUISE MISSILE
Gu Wenjin Navy Aeronautic Engineering Institute.STATIC AND DYNAMIC ADJUSTMENT OF SIX-DEGREE-OF-FREEDOM SIMULATION SYSTEM FOR CRUISE MISSILE[J].Tactical Missile Technology,1991(1):23-28.
Authors:Gu Wenjin Navy Aeronautic Engineering Institute
Affiliation:Gu Wenjin Navy Aeronautic Engineering Institute
Abstract:The three-channel hardware-in-the-loop flight simulation subsystem in the "simulation engineering for navy missile weapon systerns" has been introduced with particular attention given to its compositions, functions as well as static and dynamic adjustment. Some experiences have been provided for simulation study of tactical cruise missiles.
Keywords:Guided missile Simulation ~#Static and dynamic adjustment
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