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UAV flight assistance method and system, UAV and mobile terminal

A mobile terminal and auxiliary system technology, applied in the field of flight auxiliary systems, can solve the problems of drones such as easy to fly, small size, and disorientation, so as to avoid blind flying and flying loss, and improve the flight experience.

Active Publication Date: 2018-09-25
SZ DJI TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

When the operator is operating a moving body, such as a drone, since the drone is generally small in size, it is difficult to see clearly with the naked eye when flying far (such as four to five hundred meters). In this case, the control It is difficult for the operator to observe the heading angle of the UAV, which is equivalent to blind flight. If there is no auxiliary means of flight, the UAV is easy to fly.
In addition, if you fly in FPV (First Person View, first-person perspective) mode, if you focus too much on the display screen, you may not be able to understand the current position of the drone in the end, resulting in disorientation or even flying, and while watching FPV , while paying attention to the position of the drone, it will greatly reduce the user experience

Method used

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  • UAV flight assistance method and system, UAV and mobile terminal
  • UAV flight assistance method and system, UAV and mobile terminal
  • UAV flight assistance method and system, UAV and mobile terminal

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Embodiment Construction

[0074] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0075] The implementation of the present invention will be described in detail below in conjunction with specific embodiments.

[0076] see figure 1 , a kind of unmanned aerial vehicle flight assistance method provided by the present invention, it comprises the following steps:

[0077] S101: Receive an instruction to execute a flight assistance function;

[0078] Please also refer to Figure 2-4 , the mobile terminal 20 sends an instruction to execute the ...

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Abstract

The invention discloses a flight assistance method and system for an unmanned aerial vehicle, an unmanned aerial vehicle and a mobile terminal. The flight assistance method of the drone includes the following steps: receiving an instruction to perform a flight assistance function; recording the position of the point of interest; recording the current location of the drone; The forward direction of the drone's flight.

Description

technical field [0001] The invention relates to a flight assistance system and method for an unmanned aerial vehicle. Background technique [0002] In recent years, unmanned aerial vehicles (such as fixed-wing aircraft, rotorcraft including helicopters) have been widely used, such as in detection, search and rescue and other fields. When the operator is operating a moving body, such as a drone, since the drone is generally small in size, it is difficult to see clearly with the naked eye when flying far (such as four to five hundred meters). In this case, the control It is difficult for the operator to observe the heading angle of the UAV, which is equivalent to blind flight. If there is no auxiliary means of flight, the UAV will be easily lost. In addition, if you fly in FPV (First Person View, first-person perspective) mode, if you focus too much on the display screen, you may not be able to understand the current position of the drone in the end, resulting in disorientati...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05D1/10B64C39/02H04M1/725G08C17/02H04M1/72415
CPCB64C39/024G05D1/101G08C17/02H04M1/72415B64U10/25B64U10/10B64U2201/20B64D43/00B64D47/08G05D1/0202G05D1/0016G05D1/0022G05D1/0038G05D1/0044B64U2201/104B64U10/13B64U2101/30G01S19/42
Inventor 宋健宇
Owner SZ DJI TECH CO LTD
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