Improved fixed wing UAV and its control and landing method

摘要

The present application provides a fixed wing unmanned aerial vehicle, which comprises: - a propulsion device (- 30,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,-At least one UAV position sensor - at least one government (21)A computing device is characterized in that the computing device is configured to drive an UAV according to a landing protocol including: - phase approach to a predetermined landing point.-A downlink phase in which the calculator controls each pointer to move the UAV in an orbit between 25 ° and 30 ° towards a predetermined landing point,There's also a controlled decoupling phaseWhen the calculator controls each pointer, the angle of the UAV is greater than 30 °, which is suitable for driving it to uncouple until the UAV lands.