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Unmanned aerial vehicle integrated navigation complex with adaptive tuning

机译：自适应调整的无人机综合导航系统

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摘要

The proposed scheme of construction of an integrated navigation complex of an unmanned aerial vehicle, the basis of which are two subsystems - inertial and course-air. For each subsystem, implementation of algorithms for the complex processing of navigation information from the corresponding navigation sensors and onboard equipment of the Global Positioning System on the basis of a non-invariant compensation circuit is envisaged. The logic of using navigation measurements from both subsystems reflects the adaptation of the navigation complex to the flight conditions of the aircraft. The adaptive navigational complex unmanned aerial vehicle will improve the accuracy of the determination of navigational parameters of the flight, reliability and noise immunity of the aircraft during the flight task.
机译：拟议的无人飞行器综合导航系统的建造方案，其基础是两个子系统-惯性和航向。对于每个子系统，设想基于非不变补偿电路对来自相应的导航传感器和全球定位系统的机载设备的导航信息进行复杂处理的算法的实现。使用来自两个子系统的导航测量值的逻辑反映了导航系统对飞机飞行条件的适应性。自适应导航复杂无人飞行器将提高在飞行任务期间确定飞行导航参数的准确性，飞机的可靠性和抗扰性。

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