一种便携式多无人机发射控制系统的设计  

Design of a portable UAV launch control system

作　　者：冷月香 刘江[2] 马远超 LENG Yue xiang;LIU Jiang;MA Yuan chao(Xi’an ASN Technology Group Co.,Ltd,Xi’an 710065,China;Northwestern Polytechnical University,Xi’an 710065,China)

机构地区：[1]西安爱生技术集团公司,陕西西安710065 [2]西北工业大学,陕西西安710065

出　　处：《电子设计工程》2019年第22期39-42,47,共5页Electronic Design Engineering

基　　金：国家重大科学仪器设备开发专项项目(2013YQ31079906)

摘　　要：依据某型多无人机系统的需求,针对系统任务的飞行前的地面保障环节,设计了多无人机便携式发射控制系统设备。该便携设备由发控计算机、硬指令键盘、发射控制软件、外接电缆等组成,发控计算机采用CPCI加固型便携式计算机,指令键盘采取STM32单片机进行编码设计,发控软件使用Microsoft Visual C++6.0编写,无人机加电后,外接电缆连接机体和发射控制系统,进行飞行前的航电设备检测、飞机性能检测、航路规划等飞前准备工作,提高飞前检测效率。经过系统联试,表明该便携式发射控制系统在多无人机系统中地面保障环节中具有快速性和便捷性。According to the requirements of a certain type of multi-UAV system,a multi-UAV Preflight ground support for system missions was designed for the pre-flight ground support link of the system mission. The portable device is composed of a control computer,a hard command keyboard,a launch control software,an external cable,etc. The control computer adopts a CPCI ruggedized portable computer,the command keyboard adopts STM32 single chip for coding design,and the control software is written by Microsoft Visual C++ 6.0. After the drone is powered on,the external cable is connected to the body and the emission control system to perform pre-flight avionics detection,aircraft performance detection,route planning and other pre-flight preparations to improve the efficiency of pre-flight detection. After the system joint test,it shows that the portable launch control system is fast and convenient in the ground support link of the multi-UAV system.

关 键 词：多无人机 便携式 发射控制系统 航电设备检测 航路规划 地面保障 

分 类 号：TP311.1[自动化与计算机技术—计算机软件与理论]