The integration test for static parameter was completed by control software as well as event-driven, callback functions and interactive program.

测控软件以事件驱动、回调函数与交互式程序，完成静态参数综合测试。

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Through calculating service temperature by flight parameter and based on the flight training program, infield and outfield test-fly program, and compares the result with actual-measurement.

包括用飞行训练大纲和内厂、外场试飞大纲作为飞行剖面编制的依据； 以飞参数据作为温度载荷的原始输入； 采用大气状态下的实测结果进行温度校正计算等。

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