无人机发动机的自动化智能测试系统  

The Automatic Intellective Measurement System of UAV's Engine Based on Microcomputer

作　　者：高翔[1] 殷业飞[1] 

机构地区：[1]空军工程大学导弹学院,陕西三原713800

出　　处：《弹箭与制导学报》2005年第SA期446-449,共4页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：以系统采用的软硬件复合抗干扰技术和大集合试车数据存储的方法为重点,从组成、工作原理和软硬件设计三个方面介绍了某型无人机发动机参数测试系统。应用微型计算机对发动机的主要试车参数进行自动化智能测试。应用表明,该系统具有性能稳定可靠,操作简单、工作效率高和能显著提高发动机试车参数测试精度的特点。Emphasized on the anti-jamming techniques of its hardware and software and the storage method of its mass trial data,three aspects which are the composition,work principle and the design of the hardware and software for pa- rameter measurement system of some kind of UAV's engine are introduced in this paper.Carry on automatic and intellec- tualized measurement on primary trial run parameter of the engine using single-chip microcomputer.Practical application shows that the system has the characters of having stable,reliable performance and being easily operated in actual appli- cation,having good effectiveness and enhancing the trial run parameter of the engine measurement accuracy of the en- gine.

关 键 词：参数测试 无人机 微型计算机 RS232接口 

分 类 号：V241.06[航空宇航科学与技术—飞行器设计]