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防空导弹制导控制系统混合计算机实时仿真
引用本文:梁炳成.防空导弹制导控制系统混合计算机实时仿真[J].战术导弹技术,1991(1):14-22.
作者姓名:梁炳成
作者单位:北京仿真中心
摘    要:本文扼要介绍了导弹制导控制系统在大型现代混合计算机上进行实时系统仿真建模、验模和运行的全过程,说明了建立实时仿真模型的重要性。文章用较大篇幅详细阐述了建立导弹飞行实时混合仿真模型时,分配数字、模拟任务和确定混合仿真帧时的原则;编程控制A/D、D/A通道数据转換,设计气动多变量函数,坐标变换实时仿真模型的方法以及仿真模型校验方法。

关 键 词:防空导弹  混合计算机  坐标变换

REAL TIME SIMULATION OF GUIDANCE SYSTEMS FOR AIR-DEFENSE MISSILE ON HYBRID COMPUTER
Liang Bingcheng The Beijing Simulation Centre.REAL TIME SIMULATION OF GUIDANCE SYSTEMS FOR AIR-DEFENSE MISSILE ON HYBRID COMPUTER[J].Tactical Missile Technology,1991(1):14-22.
Authors:Liang Bingcheng The Beijing Simulation Centre
Affiliation:Liang Bingcheng The Beijing Simulation Centre
Abstract:The whole process of real time modelling, verification and simulation on modern large-scale hybrid computer for missile guidance systems has been described briefly, and the importance of the real time modelling is discussed. The test assignment for digital computation and analog computation, determination of frame time for hybrid simulation, control of A/D, D/A data conversion, treatment of multivariable aerodynamic functions, coordinate transformation, and model verification are mainly stressed as for real time simulation.
Keywords:Antiaircraft missile Hybrid computer Coordinate transformation
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