An aircraft stand control system and method

Abstract

The invention discloses a method and system for controlling an aircraft tripod. Including: the tripod control module controls the tripod drive motor to drive the deployment of the aircraft tripod. When the aircraft tripod is deployed to the support position, the tripod control module controls the tripod drive motor to stop driving the aircraft tripod to continue to unfold; the tripod control module controls The tripod drive motor drives the aircraft tripod to retract. When the aircraft tripod is retracted to the retracted position, the tripod control module controls the tripod drive motor to stop driving the aircraft tripod to continue retracting. The invention realizes that the tripod of the aircraft can be stored for easy storage when not in use, and the tripod can be automatically recovered during the flight without disturbing the aerial detection and other work of the aircraft. Combined with the altitude feedback of the altitude detection module or the remote control of the remote controller, the aircraft can automatically deploy the aircraft tripod to the support position in time before landing, thereby providing a reliable guarantee for the stable support of the aircraft on the landing surface.

Description

technical field [0001] The invention relates to aircraft manufacturing technology, in particular to an aircraft foot stand control method and system capable of controlling the deployment and recovery of the aircraft foot stand. Background technique [0002] At present, aircraft or unmanned aerial vehicles have been more and more widely used in social life, for close-range observation of places that are difficult for people to reach, or for high-altitude aerial photography, which provides convenience for observation and shooting. [0003] Existing aircraft often consists of an aircraft fuselage and a machine arm extending from the aircraft fuselage to the outside. Motors and propellers are installed at the outer ends of the machine arms to drive the flight of the aircraft. A tripod is also provided at the bottom of the aircraft. to facilitate the landing of the aircraft. [0004] However, in the existing aircraft, the stretched arms and tripods are all fixedly connected to t...

AI Technical Summary

Problems solved by technology

[0006] In view of this, the present invention provides an aircraft stand control method and system to realize the automatic opening and closing of the aircraft stand, and solve the problems of inconvenient storage and flight control caused by the failure of the existing aircraft stand to open and close.

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