Unmanned aerial vehicle integrated navigation complex with adaptive tuning

Abstract

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.