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Unmanned aerial vehicle safety test system and method

A technology for unmanned aerial vehicles and safety testing, which is applied in the field of unmanned aerial vehicles and can solve the problems of low safety in the testing process of unmanned aerial vehicles

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

AI Technical Summary

Problems solved by technology

[0004] The main purpose of the present invention is to provide a safety testing system and method for unmanned aerial vehicles, aiming at solving the technical problem of low safety in the testing process of unmanned aerial vehicles in the prior art

Method used

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  • Unmanned aerial vehicle safety test system and method
  • Unmanned aerial vehicle safety test system and method
  • Unmanned aerial vehicle safety test system and method

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Embodiment Construction

[0061] It should be understood that the specific embodiments described herein are only used to explain the present invention, but not to limit the present invention.

[0062] refer to Figure 1 to Figure 5 , Figure 1 to Figure 5 This is a schematic diagram of a test scene of an embodiment of the unmanned aerial vehicle safety test system of the present invention.

[0063] The unmanned aerial vehicle safety testing system 100 includes: a safety connection assembly 10, a flight track 20, a central controller 1 and an unmanned aerial vehicle 40, wherein the central controller 1 is in communication connection with the unmanned aerial vehicle 40, and the The unmanned aerial vehicle 40 is connected with the flight track 20 through the safety connection assembly 10;

[0064] It should be noted that this embodiment is applied to the test process of the unmanned aerial vehicle 40, and the unmanned aerial vehicle 40 may be an unmanned aerial vehicle or other unmanned aerial device wi...

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Abstract

The invention belongs to the field of unmanned aerial vehicles, and discloses an unmanned aerial vehicle safety test system and method. The system comprises a central controller, a flight track, a safety connection assembly and an unmanned aerial vehicle. The safety connecting assembly is connected with the unmanned aerial vehicle and the flight track; the flight track is in an activity area limiting the unmanned aerial vehicle; the central controller generates aircraft test parameters; the unmanned aerial vehicle performs a flight test according to the aircraft test parameters to obtain flight test data; and the central controller generates a test result according to the flight test data. According to the scheme, an aircraft safety test track and a closed safety test site are constructed. And it can be ensured that the aircraft completes various key performance tests in an absolutely safe environment. The test safety is improved, the unmanned aerial vehicle cannot fall and be damaged when being out of control, the safety of the unmanned aerial vehicle for testing is guaranteed while the test effect is not hindered, and the potential safety hazard of the test is reduced.

Description

technical field [0001] The present invention relates to the technical field of unmanned aerial vehicles, in particular to a safety testing system and method for unmanned aerial vehicles. Background technique [0002] The initial design of the aircraft is completed, and the test has verified that the risk of crash is extremely high. When a power system failure occurs, the aircraft will fall directly from the air, posing a safety risk to the surrounding people. When the flight control system of the aircraft fails, the aircraft will fly to an unpredictable area, causing serious social security risks. [0003] The current aircraft test technology generally adopts indoor simulated flight test, but the key function tests of the aircraft cannot be completed indoors due to site restrictions. Routes, wind resistance, loading capacity, etc. cannot be tested in practice. If an outdoor flight test is used, there may be a safety risk of crashing, and unmanned aerial vehicles may run out...

Claims

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Application Information

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IPC IPC(8): B64F5/60
CPCB64F5/60B64U10/10
Inventor 张叶张进刚
Owner SICHUAN AEE AVIATION TECH CO LTD
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