| 导弹速率捷联姿态控制系统三通道半实物仿真试验方法研究 |
| |
| 引用本文： | 龚汉兵.导弹速率捷联姿态控制系统三通道半实物仿真试验方法研究[J].系统工程与电子技术,1992(9). |
| |
| 作者姓名： | 龚汉兵 |
| |
| 作者单位： | ○六六基地 |
| |
| 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。
|
| 关 键 词： | 捷联式惯性制导 姿态控制系统 捷联式陀螺 模拟试验 试验方法 战术弹道导弹 |
Three-Channel Simulation Test Method of Missile Rate Strap-Down Attitude Control System |
| |
| Gong HanbingHubei Yuanfang Industry Corporation.Three-Channel Simulation Test Method of Missile Rate Strap-Down Attitude Control System[J].System Engineering and Electronics,1992(9). |
| |
| Authors: | Gong HanbingHubei Yuanfang Industry Corporation |
| |
| Institution: | Gong HanbingHubei Yuanfang Industry Corporation |
| |
| Abstract: | 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. |
| |
| Keywords: | Rate strap-down attitude control Simulation test Method |
| 本文献已被 CNKI 等数据库收录！ |
