某型飞机导弹靶试航迹测量的论证与实施  

Practicability and Implementation of an Airborne Instrumentation System for Missile Bore sighting Tests

作　　者：杨雨松[1] 祖力军[1] 陈明[1] 

机构地区：[1]中国人民解放军驻沈阳飞机工业(集团)公司军事代表室,沈阳110035

出　　处：《飞机设计》2003年第3期73-77,共5页Aircraft Design

摘　　要：论述了空中靶试遥测改装方案的可靠性、安全性、可操作性及测试原理 ,对代用天线与测试设备天线使用频段的兼容性进行了对比分析。某型导弹靶试项目是某机种首次进行的空中试验任务 ,是提升我军战斗能力 ,武器国产化能力的一个重要项目。为保证此项目的完成 ,需对武器发射后的运行轨迹、击中目标后的精度进行遥测。为了保证测试任务的完成 ,相关专家对机上加装的遥测设备进行了充分的论证 ,保证了靶试成功。An airborne instrumentation system was designed for a missile bore sighting flight test program that has been being performed to improve the combat effectiveness of a type of fighter aircraft and enhance the weapon localization ability The practicability of the instrumentation system was discussed in terms of reliability, safety, operability and testing theory. The compatibility between the antenna substitutes and onboard equipment in their operation frequency band was analyzed. The installation of the system hard wares in the aircraft and the ground test and flight demonstration of the system are also presented.

关 键 词：飞机 导弹空中靶试 航迹测量 运行轨迹 机载设备 GPS 

分 类 号：V271.4[航空宇航科学与技术—飞行器设计] TJ760.62[兵器科学与技术—武器系统与运用工程]