Auxiliary take-off and landing device for aircraft and landing and take-off control method thereof

Abstract

The invention provides an auxiliary takeoff and landing device for an aircraft, and further provides a landing and takeoff control method of the auxiliary takeoff and landing device for the aircraft.The auxiliary takeoff and landing device comprises a magnetic part and a landing assembly. The landing assembly is provided with a landing surface, a magnetization part and a demagnetization part. When the magnetization part enters the magnetic field range of the magnetic part, the magnetic part can magnetize the magnetization part, and thus magnetic attraction force is generated between the magnetic part and the magnetization part. When the aircraft is started up to start propellers, the demagnetization part can eliminate or weaken the magnetic attraction force between the magnetic part and the magnetization part. The magnetic part is arranged on the aircraft and matched with the landing surface, the magnetization part and the demagnetization part of the landing assembly not on the aircraft, so that attraction fixing during aircraft landing and attraction force eliminating or weakening when the aircraft is started up to start the propellers are achieved, the aircraft is assisted to take off and land automatically, landing fixing and reliability are ensured, and thus the performance of the aircraft is ensured.

Description

technical field [0001] The invention relates to the technical field of aircraft equipment, in particular to an aircraft auxiliary take-off and landing device and a landing and take-off control method thereof. Background technique [0002] At present, unmanned aerial vehicles can realize automatic control in various links such as take-off and landing, and there is less and less human intervention. Since the unmanned aerial vehicle may not be recovered immediately after landing, considering the light weight of the unmanned aerial vehicle itself, the unmanned aerial vehicle will move and roll over under the action of the wind after landing, causing damage to the unmanned aerial vehicle, and, The unmanned aerial vehicle will also be affected by the wind force during the landing process, which will affect the stability of the unmanned aerial vehicle's landing. Therefore, when the unmanned aerial vehicle lands, there will be a problem of position deviation, which will affect the ...

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Problems solved by technology

[0003] Based on this, it is necessary to address the problem of the performance of the aircraft caused by the deviation of the position of the current unmanned aerial vehicle when it lands, and provide an auxiliary take-off and landing device for the aircraft that can assist the aircraft to land, ensure that the aircraft lands and is fixed and reliable, and also provide an application. A landing control method for an auxiliary take-off and landing device for an aircraft, and a take-off control method using the above-mentioned auxiliary take-off and landing device for an aircraft

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