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飞机的姿态角和航向角参数是磁航向姿态基准系统中重要的飞行姿态参数,包括姿态陀螺的俯仰角、倾斜角和航向陀螺的航向角,这些对于保障飞行安全,提高飞行训练水平和机务维护质量都具有十分重要的作用。本论文在分析同步器信号转换板为硬件主体,采用LabWindows/CVI虚拟测试设备多线程编程技术的基础上,详细介绍LabWindows/CVI实现某型磁航向基准系统信号角度A/D解算的编程思路及过程。
The aircraft attitude and heading parameters are the important flight attitude parameters in the magnetic heading attitude reference system, including the pitch angle and inclination angle of the attitude gyroscope and the heading angle of the heading gyroscope. These are very important for ensuring flight safety, improving flight training level and maintenance of aircraft Quality has a very important role. Based on the analysis of multithreaded programming technology of LabWindows / CVI virtual test equipment, this paper introduces the programming principle of LabWindows / CVI to realize A / D solution of signal angle of a certain magnetic heading reference system And the process.