Aircraft today use complex avionic systems .

当今的飞机使用复杂的电子控制系统。

The thesis provides a theoretical basis and key parameters for the full implementation of avionics partition management . It is helpful to establish the safity critical avionic systems , and lay a foundation for the avionics software integration .

本文的结论将有助于航空电子分区管理，为全面实施分区策略提供理论依据和实施关键参数，为综合化航空电子系统的软件集成奠定了基础。

Measuring and computing air data is an indispensable factor in avionic systems , and the related air-data computation system has become an important part of the flight instruments .

大气飞行数据的量测以及计算是一项航空工程不可或缺的要素，而其对应的数据仪表系统也是飞行状态仪表的重要部分之一。

The paper applied the integration environment to task computer of some an avionic , heat designed and analyzed the computer , and predicted it , tested project application of the integration environment .

文中将该集成环境应用在航空某型号任务计算机中，对任务计算机进行了热设计、热分析和可靠性预计，测试了集成环境的工程实用性。