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飞行模拟器滑油压力表仿真器设计
引用本文:王述运,林亚军,魏青,田杰荣.飞行模拟器滑油压力表仿真器设计[J].自动化与仪表,2012,27(5):13-16.
作者姓名:王述运  林亚军  魏青  田杰荣
作者单位:海军飞行学院模拟中心,葫芦岛,125001
摘    要:针对某型飞机飞行模拟器仪表系统的特点,以滑油压力表为例,对常用电流比值表仿真器进行了研究,提出了利用同步器代替实装传感器的实施方案,并给出了基于CAN总线的同步器实现方法。实践证明,该仿真器精度高、实时性强、扩展灵活,具有通用性和实用性等特点。

关 键 词:飞行模拟器  滑油压力表  电流比值表  CAN总线  分段线性插值法

Design of Oil Pressure Indicator Emluator for Flight Simulator
WANG Shu-yun , LIN Ya-jun , WEI Qing , TIAN Jie-rong.Design of Oil Pressure Indicator Emluator for Flight Simulator[J].Automation and Instrumentation,2012,27(5):13-16.
Authors:WANG Shu-yun  LIN Ya-jun  WEI Qing  TIAN Jie-rong
Affiliation:(Department of Simulating,Navy Flying Academy,Huludao 125001,China)
Abstract:According to the characteristics of the instrument system for a certain type flight simulator,the oil pressure indicator was used as an example to research electric current ratio instrument emluator.The implementation plan used synchronizer instead of original sensor was present and the design method based on CAN-bus was described.The practice indicates that the proposed methods can achieve high precision,better real-time and extensibility.These methods gain favorable effects in the exploitation of practical projects.
Keywords:flight simulator  oil pressure indicator  electric current ratio instrument  CAN-bus  divided linear difference method of interpolation
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