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基于DSP的数字航姿模拟器设计
引用本文:李禾 李尚柏 周维 郑高群. 基于DSP的数字航姿模拟器设计[J]. 微计算机信息, 2007, 23(1Z): 207-209
作者姓名:李禾 李尚柏 周维 郑高群
作者单位:成都市四川大学原子核科学技术研究所辐射物理及技术教育部重点实验,四川成都610064
摘    要:
航姿模拟器是在对机栽设备进行地面测试时用来仿真飞机航姿信号的专门设备。传统航姿模拟器通用性差、控制精度低且不易与自动测试系统(ATE)接口。为此设计了基于DSP的数字航姿模拟器。该模拟器能同时输出航向、横滚及俯仰信号,可与计算机接口或直接嵌入自动测试系统,具有跟踪速度快、精度高、控制简单等特点。该模拟器在某型机载雷达ATE中获得应用。

关 键 词:数字航姿模拟器 DSP AD5547 频率跟踪算法 雷达ATE
文章编号:1008-0570(2007)01-2-0207-03
修稿时间:2006-06-272006-07-25

A DSP based digital flight attitude simulator design
LI HE LI SHANGBAI ZHOU WEI ZHENG GAOQUN. A DSP based digital flight attitude simulator design[J]. Control & Automation, 2007, 23(1Z): 207-209
Authors:LI HE LI SHANGBAI ZHOU WEI ZHENG GAOQUN
Abstract:
Flight attitude simulators are special devices to generate flight attitude signals for aircraft carried equipments ground testing. The traditional analog simulators are low precision, not generally applicable for different type of equipment and difficulty to interface to ATE, Thus a DSP based digital flight attitude simulator was designed. The simulator can generate high precision flight heading, rolling and pitch signals simultaneously with fast tracking speed. And it also can be connected to computer or embedded into an ATE system for easy control. The simulator has been successfully used in a radar ATE.
Keywords:digital flight attitude simulator  DSP  AD5547  algorithm for frequency tracking  radar ATE
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