Telemetry data driven unmanned plane flight state identification method

A technology of telemetry data and flight status, which is applied in navigation computing tools and other directions, and can solve problems such as inconsistent data length, large data volume, and uneven distribution of type samples

Active Publication Date: 2016-12-07
HARBIN INST OF TECH
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  • Application Information

AI Technical Summary

Problems solved by technology

[0052] The purpose of the present invention is to solve the problems of large amount of sample data, non-uniform data length and uneven distribution of various types of samples in the identification of UAV flight status, and then provide a remote measurement data-driven UAV flight status identification method

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  • Telemetry data driven unmanned plane flight state identification method
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  • Telemetry data driven unmanned plane flight state identification method

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Embodiment Construction

[0113] The present invention will be described in further detail below in conjunction with the accompanying drawings: the present embodiment is implemented on the premise of the technical solution of the present invention, and detailed implementation is provided, but the protection scope of the present invention is not limited to the following embodiments.

[0114] Chebyshev Fitting Algorithm and Random Forest Algorithm

[0115] Based on Chebyshev Feature Extraction-Random Forest Classification Algorithm (C-RF Algorithm)

[0116] At present, during the flight of UAVs, the main basis for monitoring the flight status of UAVs is the telemetry data transmitted by the UAV to the ground, which is the time series data generated by the on-board sensor measurement and control system. The duration of different flight states of the UAV is different during each flight, and the length of the multidimensional time series corresponding to each sample is also different, so it is difficult to ...

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Abstract

The invention provides a telemetry data driven unmanned plane flight state identification method, and provides a Chebyshev-random forest algorithm (C-RF) unmanned plane state identification method. The telemetry data of an unmanned plane undergoes characteristic extraction and dimension reduction through adopting a Chebyshev fitting technology, and the adaptive classification of the flight state is realized by using a random forest algorithm. The method combines the advantages of simple calculation and optimum fitting approaching of a Chebyshev fitting coefficient with the advantages of fast training speed, high classification accuracy and strong noise resistance, can cover various samples of the unmanned plane and avoid an over-fitting problem, and realizes effective identification of the flight state of the unmanned plane. Real unmanned plane flight telemetry data is adopted to carry out identification, so the total identification accuracy is higher than 90%, and a small amount of kinds of the samples is accurately identified, so the effectiveness and the practicality of the method are proved.

Description

technical field [0001] The invention relates to a method for identifying the flight state of an unmanned aerial vehicle driven by telemetry data, and belongs to the technical field of identification methods for the flight state of an unmanned aerial vehicle. Background technique [0002] UAV (Unmanned Aerial Vehicle, UAV) is a reusable unmanned aerial vehicle, which is usually controlled by radio remote control equipment or operated by an onboard program to achieve flight. The flight state is an abstract description of different flight behaviors during the flight of the UAV, which can be simplified to several standard states, such as climbing, level flight, circling, turning, and descending. The real flight process of the UAV is composed of continuous conversion or combination of different flight states. Through the recognition of the flight state of the UAV, the real flight state change of the UAV can be obtained, and the task completion of the UAV during the flight can be...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01C21/20
CPCG01C21/20
Inventor 彭宇贺思捷刘大同王文娟彭喜元
Owner HARBIN INST OF TECH
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