标准摘要
[中文适用范围]： 主要面向飞行器导航与飞控系统的开发与验证阶段，为工程技术人员提供了具体的技术指导和参考框架。该规范经过严格的行业审查程序，反映了当时航空电子技术的先进水平。 ***此介绍可能不准确，请注意参考原文。 [外文原描述]： This Standard covers air data equipment (hereinafter designated the instrument) which when connected to sources of aircraft electrical power, static pressure, total pressure and outside air temperature (singly or in combination) provides some or all of the following computed air data output signals:Pressure Altitude *Total Temperature *Pressure Altitude (Reporting)Altitude RateBaro-Corrected Pressure Altitude *Overspeed WarningVertical Speed *Altitude HoldComputed Airspeed *Airspeed HoldMach Number *Mach HoldMaximum Allowable Airspeed *q c (impact pressure)Static Air Temperature ( * when used as an alternate for total temperature)True Airspeed OthersCross Reference: NASA/TN-D822,RTCA/DO-138,TSO-C-88
英文名称Air Data Computers, MPS