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 .
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 .
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 .
