摘要
本文提出了导弹速率捷联姿态控制系统三通道仿真试验中不需要三轴模拟飞行转台参与的试验方法,论述了试验原理、试验编排程序和试验步骤。举出了某战术地地导弹速率捷联姿态控制系统仿真试验实例及其飞行试验结果来说明试验原理的正确性、方法的可行性和适用性。研究表明:导弹速率捷联姿态控制系统三通道仿真试验,按本文提出的方法实施,可以简化试验程序,节省试验周期和经费,提高试验效率,获得满意的试验结果。
This article presents a three-channel simulation test method without triaxle flight simulation turntable involved in. it describes principle, program and procedure of the test. An example of the simulation test of one tactical surface-to-surface missile rate strap-down attitude control system and its flight test result are given to prove the correctness of the principle, the feasibility and applicability of the method. It shows that with respect to the three-channel simulation test of missile rate strap-down attitude control system, the method mentioned above can simplify the procedure, save the time and cost, improve the effect and give a satisfactory result.
出处
《系统工程与电子技术》
EI
CSCD
1992年第9期35-40,60,共7页
Systems Engineering and Electronics
关键词
导弹
控制系统
模拟试验
仿真
Rate strap-down attitude control, Simulation test, Method.
