航天测量船机载校飞系统构建  

Construction of Airborne Calibration System for Tracking and Controlling Ship

作　　者：霍立平[1] 贾绍文[1] 江志东[1] 蔡慧敏[1] HUO Li-ping;JIA Shao-wen;JIANG Zhi-dong;CAI Hui-min(Qingdao Branch, Naval Aeronautical and Astronautical University, Qingdao 266041, China)

机构地区：[1]海军航空工程学院青岛校区

出　　处：《仪表技术》2018年第2期41-42,46,共3页Instrumentation Technology

摘　　要：为了对航天测量船进行海上动态校飞,需在飞机上搭载合作目标,构建校飞系统。介绍了校飞原理及机载校飞系统的组成;提出了飞机改装的设计原则;给出了总体布置及供电设计;分析了全机电磁兼容性和安全性。实践表明,机载校飞系统满足使用需求。In order to carry out dynamic calibration flight for tracking and controlling ship,the airborne calibration system is built by carrying the cooperation target on the aircraft. The principle and composition of calibration flight is introduced. The design principle of aircraft modification is proposed. Overall arrangement and power supply design are given. Electromagnetic compatibility and safety is analyzed. Flight test shows that the airborne calibration system meets the requirements.

关 键 词：校飞 改装 电磁兼容性 

分 类 号：V243[航空宇航科学与技术—飞行器设计]