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A short-distance sliding method for unmanned aerial vehicles

A technology of unmanned aerial vehicles and tobogganing, which is applied in the direction of non-electric variable control, instruments, control/regulation systems, etc., which can solve the problem of unmanned aerial vehicles landing in unknown places, difficulties in unmanned aerial vehicle search work, and excessive requirements for personnel environment and site and other issues to achieve the effect of ensuring safe landing, small site demand, and reducing damage

Active Publication Date: 2018-07-10
深圳飞马机器人科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

If the operator is inexperienced, the drone may land in an unknown place under the influence of a slight wind
Although under the protection of the parachute, it will not hurt people, but the search work of the drone is quite difficult
[0007] To sum up, the current landing methods of fixed-wing UAVs place too many requirements on the personnel and environment.

Method used

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  • A short-distance sliding method for unmanned aerial vehicles

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Embodiment Construction

[0018] The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0019] This embodiment provides a short-distance sliding method for unmanned aerial vehicles, such as figure 1 As mentioned above, first, after the UAV enters the automatic downhill logic, the UAV will plan a circular circling path at the center of the circle based on the midpoint coordinates of the given taxiing track, and perform fixed-point circling over the midpoint coordinates of this track . After the hovering height is stable, the UAV will automatically descend to a safe height while circling.

[0020] When the height of the UAV is completed and stabilized, the flight control system of the UAV will plan a rectangular four-sided route with the set landing route as the final side, that is, the taxi track as the fourth side of the four-sided route. When the drone's nose pointing direction is in the same direction as the starting side of...

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Abstract

The invention discloses a short-distance slide landing method of an unmanned aerial vehicle. The short-distance slide landing method comprises the steps of S1, entering an automatic slide landing function; S2, making the unmanned aerial vehicle fly above a preset slide landing track; S3, reducing the height of the unmanned aerial vehicle, and determining a fact that the height of the unmanned aerial vehicle reaches a lower limit of a safe height; S4, planning a four-side course and utilizing the slide landing track as the fourth side of the four-side course; S5, making the head of the unmanned aerial vehicle be same with the first side of the four-side course and making the unmanned aerial vehicle fly according to the four-side course; S5, reducing the rotation speed of an engine when the unmanned aerial vehicle flies to the third side of the four-side course; S6, after the unmanned aerial enters the fourth side of the four-side course, namely the slide landing track, shutting down the engine, reducing a pitch angle and reducing the height of the unmanned aerial vehicle in a diving manner; S7, determining a fact that the height of the unmanned aerial vehicle is lower than the safe height; S8, reducing the speed of the unmanned aerial vehicle and controlling a flight direction; and S9, realizing safe landing of the unmanned aerial vehicle. The short-distance slide landing method has advantages of no requirement for experience and control of a controller, basically no influence by abnormal weathers, and relatively low requirement for a place.

Description

technical field [0001] The invention relates to the field of unmanned aerial vehicles, in particular to a short-distance downhill method for unmanned aerial vehicles. Background technique [0002] The current landing methods for fixed-wing UAVs are mainly: [0003] (1) The pilot controls the fixed-wing aircraft to land normally [0004] (2) The pilot judges the wind direction in the air, relies on his own experience, and manually controls the parachute device through the remote control to achieve the parachute mode [0005] Among the above methods, the first method requires the drone operator to have strong control ability and experience. Especially in the environment of abnormal weather, since people can only judge the flight status of the UAV by the external environment, if the operator makes a wrong operation, it may damage the UAV or even cause harm to the ground personnel. [0006] The second method puts higher requirements on the operator, not only to estimate the d...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05D1/10
CPCG05D1/101
Inventor 程浩
Owner 深圳飞马机器人科技有限公司
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