航空测试仪器中的PC104总线技术  

PC104 Bus Technology in the Aeronautic Testing Instruments

作　　者：杨军锋[1] 朱家海[1] 谢红星[1] 

机构地区：[1]空军工程大学工程学院,陕西西安710038

出　　处：《空军工程大学学报（自然科学版）》2000年第4期13-16,共4页Journal of Air Force Engineering University(Natural Science Edition)

摘　　要：小型化与便携是航空测试仪器设计所追求的目标。针对 PC1 0 4总线系统具有体积小、结构紧凑等特点 ,在设计航空设备内场检查仪的测试电路时 ,采用了 PC1 0 4总线技术的原理和方法 ,并从工程实践出发 ,成功地解决了总线冲突与抗干扰问题。设计的结果表明 ,该检查仪具有体积小、重量轻。Miniaturization and portability are the targets in the design of the aeronautic testing instruments.For the advantages of PC104 bus system such as its small volume and compact structure,the principles and the method of PC104 bus technology are applied during the design for testing circuit in an in field testing instrument of an aeronautic equipment.And the problems such as anti jamming and the bus conflict are solved successfully in the engineering practice.The design results show that the designed testing instrument has the strong points of small volume,lightweight and exact testing result.

关 键 词：PC104总线 伺服放大器 内场检查仪 

分 类 号：N55[自然科学总论]