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Ground flight test platform and test method for coaxial double-rotor unmanned aerial vehicle

A coaxial dual-rotor, flight test technology, applied in the direction of aircraft component testing, etc., can solve the problems of lack of flight data upload processing and storage, inability to collect UAV flight data, and excessive six-freedom of the platform. The effect of measuring requirements, reducing the complexity of the mechanism, and high precision

Active Publication Date: 2019-12-24
BEIJING JIAOTONG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, due to the special structure of the coaxial dual-rotor UAV, it will not perform complex maneuvers like the multi-rotor UAV during flight. Therefore, the six degrees of freedom of the platform appear to be too much.
[0004] 2. Most existing platforms do not have sensors installed and cannot collect flight data of UAVs
[0005] 3. A small number of platforms equipped with sensors do not have the function of uploading the collected flight data to the host computer for processing and saving

Method used

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  • Ground flight test platform and test method for coaxial double-rotor unmanned aerial vehicle
  • Ground flight test platform and test method for coaxial double-rotor unmanned aerial vehicle
  • Ground flight test platform and test method for coaxial double-rotor unmanned aerial vehicle

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Experimental program
Comparison scheme
Effect test

Embodiment 1

[0065] Embodiment 1: as figure 1 , figure 2 , image 3 , Figure 4 , Figure 5 , Image 6 , Figure 7 , Figure 8 and Figure 9 As shown, a coaxial dual-rotor UAV ground flight test platform includes a mechanical part and a control part, and the control part includes a hardware module and a software module.

[0066] The mechanical part includes a frame part, a main part and a limit part, and the main part is placed on the upper part of the frame. The limiting part is connected with the main part.

[0067] The frame part includes a support frame and a support plate 27, the support frame is welded by 4 first steel pipes 14, 4 second steel pipes 22 and 4 third steel pipes 26, and the 4 second steel pipes 22 are welded into a chassis, each One end of the second steel pipe 22 has an extension end, and four third steel pipes 26 are welded on the chassis. 14 welding.

[0068] The support plate 27 is placed on the top of the four first steel pipes 14 forming a rectangle. ...

Embodiment 2

[0109] Embodiment 2: A method for ground flight testing of a coaxial dual-rotor UAV, comprising the following steps;

[0110] Taking the test of coaxial dual-rotor UAV as an example, the specific operation process of the above-mentioned coaxial dual-rotor UAV ground flight test platform is as follows:

[0111] Before starting the equipment, add some sandbags to the second steel pipe 22 to prevent the platform from moving when the UAV is flying; connect the coaxial dual-rotor UAV to the UAV connecting seat 6; check whether parts of the platform are loose, etc. Situation; Calibrate the tension sensor 5 and the torque sensor 7; Connect each module of the sensing part with the development board according to the design scheme.

[0112] Turn on the power of the development board and run the host computer program. The two are initialized respectively to check whether the Bluetooth communication between the development board and the host computer is normal, and whether the data acqui...

Embodiment 3

[0128] Embodiment 3: as figure 1 , figure 2 , image 3 , Figure 4 , Figure 5 , Image 6 , Figure 7 , Figure 8 and Figure 9 As shown, a coaxial dual-rotor UAV ground flight test platform aims to reduce the degree of freedom of the platform, simplify the mechanical structure; add a variety of sensors, write data acquisition programs; add data receiving and data processing functions, etc. to reduce the Platform production costs, adding platform functionality.

[0129] A coaxial dual-rotor unmanned aerial vehicle ground flight test platform includes a mechanical part, a sensing part, a data receiving part and a data processing part. The sensor of the sensing part is placed in the mechanical part, and stm32 is used for data collection.

[0130] The above-mentioned ground flight test platform for ground drones includes mechanical parts, sensing parts, data receiving and data processing parts. The data receiving and data processing part uses the HC05 Bluetooth module...

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Abstract

The invention discloses a ground flight test platform and test method for a coaxial double-rotor unmanned aerial vehicle and relates to the technical field of unmanned aerial vehicle tests. The groundflight test platform comprises a mechanical part and a control part. a sensor is arranged on the mechanical part, and data are collected through stm32. According to data receiving and data processingparts, the data are received by an HC05 Bluetooth module, and operation is conducted through an upper computer. The ground flight test platform comprehensively applies knowledge of the mechanical, sensing and software fields, specific to the flight characteristics of the coaxial double-rotor unmanned aerial vehicle, the mechanical structure of the platform is simplified, and data collection and data processing functions are added. Flight parameters of the unmanned aerial vehicle can be detected in real time while the unmanned aerial vehicle is protected, and later adjustment is facilitated. The sensor is replaced, thus the ground flight test platform can meet the requirements of different types of unmanned aerial vehicles and detection tasks of different measuring ranges, and good applicability is achieved.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicle testing, in particular to a ground flight testing platform and testing method for a coaxial double-rotor unmanned aerial vehicle. Background technique [0002] There are many types of existing UAV ground flight test platforms, and their structures are relatively similar, that is, they consist of a frame fixed on the ground and several rotating parts and telescopic parts. A few platforms will add sensors to collect some flight parameters. The above scheme has the following problems: [0003] 1. Existing platforms are mostly designed for multi-rotor drones, generally with six degrees of freedom. However, due to the special structure of the coaxial dual-rotor UAV, it will not perform complex maneuvers like multi-rotor UAVs during flight, so the platform has too many six degrees of freedom. [0004] 2. Most of the existing platforms are not equipped with sensors and cannot collect t...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F5/60
CPCB64F5/60
Inventor 常秋英杨密栋
Owner BEIJING JIAOTONG UNIV
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