火力与指挥控制Issue(12)：167-170,4.
制导火箭弹飞行控制半实物仿真系统设计
Design of Hardware-in-the-Loop Simulation of Flight Control System for Guided Rocket
杨永亮 1吴小役 1李颖 1王斌翊1
作者信息
- 1. 西北机电工程研究所，陕西 咸阳 712099
- 折叠
摘要
Abstract
Flight control system is a key sector of intelligent precision guided rocket. Using Rapid Control Prototype method,a hardware-in-the-loop simulation platform of flight control system for guided rocket is constructed in this paper. Through this platform,the model of control law algorithm can be downloaded to the flight control computer to achieve hardware-in-the-loop simulation,which makes it possible to design and testify the control strategy before the hardware is available. Based on analyzing the simulation experiments,it also makes contributes to the design,modification and optimization of the control software. Experiments eventually show that the platform could run stably and reliably,and has explicit real-time capability while having engineering applicable value.关键词
制导火箭弹/飞行控制/半实物仿真/快速控制原型Key words
guided rocket/flight control/hardware-in-the-loop simulation/rapid control prototype分类
军事科技引用本文复制引用
杨永亮,吴小役,李颖,王斌翊..制导火箭弹飞行控制半实物仿真系统设计[J].火力与指挥控制,2013,(12):167-170,4.
