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Display device for carrying out unmanned aerial vehicle flight verification on very-high-frequency omnidirectional range

An omnidirectional beacon and display device technology, which is applied in the field of aircraft flight verification, can solve the problems of inability to meet flight verification requirements, affecting verification results, and difficulty in meeting flight accuracy requirements for unmanned aerial vehicles.

Inactive Publication Date: 2020-04-10
北京航空航天大学东营研究院
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  • Abstract
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] Flight verification has high precision requirements for the flight trajectory of the aircraft, and when using UAVs for flight verification, it is generally difficult for UAVs to meet the flight accuracy requirements, thus failing to meet the flight verification requirements, which directly affects the verification result

Method used

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  • Display device for carrying out unmanned aerial vehicle flight verification on very-high-frequency omnidirectional range

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Embodiment Construction

[0020] 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.

[0021] The purpose of the present invention is to provide a display device for UAV flight verification for VHF omnidirectional beacons, so as to solve the problems existing in the prior art, so that the driver of the UAV can intuitively, clearly and accurately understand the The real-time status of the man-machine flight is used to adjust the flight status of the UAV in real time to ensure that the UAV flies in accordance with the standard requirements, and at ...

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Abstract

The invention discloses a display device for carrying out unmanned aerial vehicle flight verification on a very-high-frequency omnidirectional range. The display device comprises a flight verificationsystem, a display instrument and a computer system, wherein every two of the computer system, the flight verification system and the display instrument are in communication connection, the display instrument comprises a VOR compass, an unmanned aerial vehicle distance display, an elevation angle indicating compass of a VOR station and a warning flag indicating lamp, the VOR compass is used for displaying a course angle and a VOR azimuth angle of the unmanned aerial vehicle, the real-time distance between the unmanned aerial vehicle and the VOR station and the elevation angle of the VOR station are obtained by calculating the accurate positioning coordinates of the unmanned aerial vehicle in flight and the position coordinates of the VOR station through the flight verification system by the computer system, the precision is high, the two parameters are specially designed for flight verification of the VOR station, it is guaranteed that the unmanned aerial vehicle flies according to a specified path, and more visual and effective guidance is provided for flight verification of the VOR station.

Description

technical field [0001] The invention relates to the field of aircraft flight verification, in particular to a display device for UAV flight verification of VHF omnidirectional beacons. Background technique [0002] Flight inspection refers to the use of flight inspection aircraft equipped with special inspection equipment to check and evaluate the quality and quality of space signals of various navigation, radar, communication and other equipment in accordance with the relevant specifications of flight inspection to ensure flight safety. tolerance, as well as the airport's arrival and departure flight procedures, and the process of issuing a flight inspection report based on the results of inspection and evaluation. Using the precise positioning of the calibration aircraft itself, the flight calibration data is obtained by comparing the collected space signal with the ideal signal that should be available at the position, and then through calibration and adjustment, the spac...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01C25/00
CPCG01C25/00
Inventor 史晓锋周林生
Owner 北京航空航天大学东营研究院
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