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Ground test system for solar unmanned aerial vehicle

A technology for solar drone and ground testing, applied in aircraft component testing and other directions, can solve the problems of harsh test conditions, long test cycle for solar drones, and poor coverage, so as to improve convenience and test coverage. Effect

Pending Publication Date: 2022-04-26
CHINA ACAD OF AEROSPACE AERODYNAMICS
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  • Summary
  • Abstract
  • Description
  • Claims
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AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to propose a test system for solar unmanned aerial vehicles, which fills the vacancy of special intelligent equipment on the ground in the general adjustment test of solar unmanned aerial vehicles and solves the general adjustment test of solar unmanned aerial vehicles in the prior art Problems with long cycle time, harsh test conditions and poor coverage

Method used

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  • Ground test system for solar unmanned aerial vehicle
  • Ground test system for solar unmanned aerial vehicle
  • Ground test system for solar unmanned aerial vehicle

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0073] Such as figure 1 As shown, a ground test system for solar-powered drones, including:

[0074] The cabinet 1 is sequentially provided with a first cabinet 2, a second cabinet 3 and a third cabinet 4 from top to bottom;

[0075] The main control and interface unit is arranged in the first chassis 2, including a main control board and an interface board, wherein the main control board is respectively connected with the solar simulator, the electronic load and the UAV through the interface board, and is used to control the solar simulation Test the drone and receive the test data of the drone;

[0076] The solar simulator is arranged in the second chassis 3 and is respectively connected to the UAV and the main control and interface unit, and is used to accept the control of the main control and interface unit to test the UAV;

[0077] The electronic load is arranged in the third chassis 4, and is respectively connected with the UAV and the main control and interface unit,...

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Abstract

The invention discloses a ground test system for a solar unmanned aerial vehicle, and the system comprises a cabinet which is sequentially provided with a first case, a second case and a third case from top to bottom; the main control and interface unit is arranged in the first case and comprises a main control board and an interface board, and the main control board is connected with the solar simulator, the electronic load and the unmanned aerial vehicle through the interface board; the solar simulator is arranged in the second case and connected with the unmanned aerial vehicle and the main control and interface unit; the electronic load is arranged in the third case and connected with the unmanned aerial vehicle and the main control and interface unit; and the heat dissipation mechanism is arranged on the cabinet. According to the ground test system, function and performance tests can be carried out on the energy system of the solar unmanned aerial vehicle on the ground, the test convenience and coverage are effectively improved, and the total adjustment test period is shortened.

Description

technical field [0001] The invention belongs to the technical field of solar unmanned aerial vehicles, and more specifically relates to a ground test system for solar unmanned aerial vehicles. Background technique [0002] Solar-powered UAV is a new type of aircraft with great development potential. It is powered by solar energy and does not need to carry any fuel. In theory, it can realize permanent air flight. Compared with conventional drones, solar-powered drones have obvious advantages and broad application prospects, and can even act as "atmospheric satellites". Because the energy source of solar drones is solar cells, the energy management system is complex, the general adjustment test is difficult, and the task load is large, and the whole system needs sufficient sunlight to work. Carry out continuous testing for a long time, and the test conditions are harsh and the coverage is poor. The current general adjustment test is divided into two parts, indoor and outdoor...

Claims

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Application Information

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IPC IPC(8): B64F5/60
CPCB64F5/60
Inventor 俱子研王欣兰根龙
Owner CHINA ACAD OF AEROSPACE AERODYNAMICS
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