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姿态控制系统数控模型仿真软件设计
引用本文:吴长才.姿态控制系统数控模型仿真软件设计[J].航天控制,1991(3).
作者姓名:吴长才
作者单位:北京航天自动控制研究所
摘    要:本文详细分析了运载火箭姿态控制系统的箭体数控模型的特点。提出运用组合算法进行运载火箭姿态控制系统数控模型仿真软件设计,介绍了箭体方程、数控差分方程常用的计算方法。所设计的仿真软件结构和处理技巧,对于缩短仿真时间,完成各种状态下的仿真任务行之有效。通过实例计算和比较,表明这些方法和措施不仅可用于全数学仿真,亦可用于半实物仿真。

关 键 词:姿态控制系统  ~+数控模型  数学模拟  软件  设计

DIGITAL CONTROL MODEL SIMULATION SOFTWARE DESIGN OF ATTITUDE CONTROL SYSTEM
Wu Changcai Beijing Aerospace Automatic control Institute.DIGITAL CONTROL MODEL SIMULATION SOFTWARE DESIGN OF ATTITUDE CONTROL SYSTEM[J].Aerospace Control,1991(3).
Authors:Wu Changcai Beijing Aerospace Automatic control Institute
Institution:Wu Changcai Beijing Aerospace Automatic control Institute
Abstract:This paper analyses in detail the features of the digital control model of vehicle bod- ies, proposes using combined algorithms to proceed simulation software design, indroduees the general computing method of vehicle body equations and difference equations of digited control. The designed simulation software structure and the presented technique are effective for performing simulation taske under different states with short simulation time. Through computation and comparsion, it is shown that the methods described in the paper can be ap- plied not only in complate mathematic simulation but also in the simulation with hardware-in-the-loop.
Keywords:Attitude control system  ~+Digital control model mathematical simulation  Software Design
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