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Unmanned aerial vehicle flight test method, system and device and readable storage medium

A flight test, UAV technology, applied in control/adjustment systems, instruments, 3D position/channel control, etc., can solve problems such as low UAV flight test efficiency

Pending Publication Date: 2022-06-24
GEER TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The main purpose of this application is to provide a UAV flight test method, system, equipment and readable storage medium, aiming to solve the technical problem of low efficiency of UAV flight test in the prior art

Method used

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  • Unmanned aerial vehicle flight test method, system and device and readable storage medium
  • Unmanned aerial vehicle flight test method, system and device and readable storage medium
  • Unmanned aerial vehicle flight test method, system and device and readable storage medium

Examples

Experimental program
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Embodiment 1

[0025] The embodiment of the present application provides a UAV flight test method, which is applied to a UAV flight test system. The UAV flight test system includes a test terminal, a real-time simulator, and an UAV to be tested. In the first embodiment of the UAV flight test method, the UAV flight test method includes:

[0026] Step S10, receiving the UAV flight parameters and the flight mission location issued by the test terminal through the real-time simulator;

[0027] In step S20, according to the UAV flight parameters, the flight mission location and the obstacle information collected by the UAV to be tested, the UAV to be tested is controlled by the real-time simulator to perform obstacle avoidance flight, until it is detected that the drone to be tested arrives at the flight mission site.

[0028] In this embodiment, it should be noted that the UAV flight test system includes a test terminal, a real-time simulator and a UAV to be tested, and the real-time simulator ...

Embodiment 2

[0033] Further, refer to figure 2 , in another embodiment of the present application, for the same or similar content as the above-mentioned first embodiment, reference may be made to the above description, and details will not be described in the following. On this basis, the real-time simulator includes a path planning module, a flight control module and an autonomous obstacle avoidance module. Obstacle information, the steps of controlling the UAV to be tested to avoid obstacle flight through the real-time simulator include:

[0034] Step S21, generating the UAV flight trajectory through the path planning module according to the UAV flight parameters and the flight mission location;

[0035] Step S22, according to the UAV flight trajectory, control the UAV to be tested to start flying through the flight control module;

[0036] Step S23, when the UAV to be tested is flying, the UAV to be tested is controlled by the autonomous obstacle avoidance module to detect the obsta...

Embodiment 3

[0061] Further, refer to image 3 , in another embodiment of the present application, for the same or similar content as the above-mentioned first embodiment, reference may be made to the above description, and details will not be described in the following. On this basis, the steps of controlling the UAV to be tested to perform obstacle avoidance flight according to the optimized UAV flight trajectory include:

[0062] Step S241, transmitting each flight path point corresponding to the optimized UAV flight trajectory to the flight control module through the path planning module;

[0063] Step S242, generating corresponding real-time flight speed information through the flight control module according to each of the flight path points;

[0064] Step S243, according to the real-time flight speed information, control the UAV to be tested to fly through the flight control module.

[0065] In this embodiment, it should be noted that the UAV flight trajectory is composed of multi...

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Abstract

The invention discloses an unmanned aerial vehicle flight test method, system and device and a readable storage medium, and is applied to an unmanned aerial vehicle flight test system, and the unmanned aerial vehicle flight test system comprises a test terminal, a real-time simulation machine and a to-be-tested unmanned aerial vehicle. The unmanned aerial vehicle flight test method comprises the following steps: receiving unmanned aerial vehicle flight parameters and a flight task place issued by the test terminal through the real-time simulation machine; and controlling the to-be-tested unmanned aerial vehicle to perform obstacle avoidance flight through the real-time simulation machine according to the flight parameters of the unmanned aerial vehicle, the flight task site and obstacle information collected by the to-be-tested unmanned aerial vehicle until the to-be-tested unmanned aerial vehicle is detected to reach the flight task site. The technical problem of low flight test efficiency of the unmanned aerial vehicle in the prior art is solved.

Description

technical field [0001] The present application relates to the technical field of unmanned aerial vehicles, and in particular, to a method, system, device and readable storage medium for flight testing of unmanned aerial vehicles. Background technique [0002] With the development of science and technology, UAV technology has also become more and more mature. At present, when conducting UAV flight tests, UAV flight tests are carried out by using virtual simulation tests and actual flight tests. Among them, virtual simulation tests are carried out. The test is usually carried out purely in the computer, and the actual simulation test is to input the mature UAV control algorithm obtained through the virtual simulation test into the UAV, and the UAV will fly autonomously, but in order to prevent the unmanned aircraft from occurring during the actual flight test. In the case of man-machine damage, a large number of virtual simulation tests are usually required to ensure that the ...

Claims

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Application Information

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IPC IPC(8): G05D1/10
CPCG05D1/101
Inventor 付磊
Owner GEER TECH CO LTD