Development of Steady Aiming System Based on Kalman Filter and Coordinate Transformation

The aiming accuracy of the Unmanned Aerial Vehicles (UAV) Steadicam head can be affected by many factors, such as the state of the UAV during the actual flight and the installation error of the system related hardware. In order to eliminate the influence of objective factors on the UAV Steadicam, a...

Full description

Bibliographic Details
Main Authors: Yufang Lu, Lisha Meng, Haihua Tang, Lei Shi
Format: Article
Language:English
Published: IEEE 2023-01-01
Series:IEEE Access
Subjects:
Online Access:https://ieeexplore.ieee.org/document/10160027/
_version_ 1797792180423622656
author Yufang Lu
Lisha Meng
Haihua Tang
Lei Shi
author_facet Yufang Lu
Lisha Meng
Haihua Tang
Lei Shi
author_sort Yufang Lu
collection DOAJ
description The aiming accuracy of the Unmanned Aerial Vehicles (UAV) Steadicam head can be affected by many factors, such as the state of the UAV during the actual flight and the installation error of the system related hardware. In order to eliminate the influence of objective factors on the UAV Steadicam, a Kalman filter aiming algorithm based on the coordinate transformation method is proposed to eliminate the attitude error of the UAV Steadicam and improve the accuracy of the system. The algorithm uses coordinate transformation to eliminate mounting errors and combines coordinate transformation and Kalman filtering methods to eliminate objective errors of the UAV in flight. The experimental simulation results show that our method can accurately give the amount of azimuth and pitch angle error compensation during the flight of the UAV, improving the accuracy of the UAV Steadicam head. Ultimately, the method is applied to the development of a real product.
first_indexed 2024-03-13T02:29:29Z
format Article
id doaj.art-bcad2e2db7d841efbc5ab21a602857e3
institution Directory Open Access Journal
issn 2169-3536
language English
last_indexed 2024-03-13T02:29:29Z
publishDate 2023-01-01
publisher IEEE
record_format Article
series IEEE Access
spelling doaj.art-bcad2e2db7d841efbc5ab21a602857e32023-06-29T23:00:28ZengIEEEIEEE Access2169-35362023-01-0111637846379410.1109/ACCESS.2023.328900610160027Development of Steady Aiming System Based on Kalman Filter and Coordinate TransformationYufang Lu0https://orcid.org/0000-0002-9053-3104Lisha Meng1https://orcid.org/0009-0008-9679-0479Haihua Tang2https://orcid.org/0009-0003-3518-089XLei Shi3Guangxi Key Laboratory of Embedded Technology and Intelligent System, Guilin, ChinaSchool of Information Science and Engineering, Guilin University of Technology, Guilin, ChinaSchool of Information Science and Engineering, Guilin University of Technology, Guilin, ChinaSchool of Science, Guilin University of Technology, Guilin, ChinaThe aiming accuracy of the Unmanned Aerial Vehicles (UAV) Steadicam head can be affected by many factors, such as the state of the UAV during the actual flight and the installation error of the system related hardware. In order to eliminate the influence of objective factors on the UAV Steadicam, a Kalman filter aiming algorithm based on the coordinate transformation method is proposed to eliminate the attitude error of the UAV Steadicam and improve the accuracy of the system. The algorithm uses coordinate transformation to eliminate mounting errors and combines coordinate transformation and Kalman filtering methods to eliminate objective errors of the UAV in flight. The experimental simulation results show that our method can accurately give the amount of azimuth and pitch angle error compensation during the flight of the UAV, improving the accuracy of the UAV Steadicam head. Ultimately, the method is applied to the development of a real product.https://ieeexplore.ieee.org/document/10160027/Attitude errorcoordinate transformationerror compensationKalman filteringSteadicam head
spellingShingle Yufang Lu
Lisha Meng
Haihua Tang
Lei Shi
Development of Steady Aiming System Based on Kalman Filter and Coordinate Transformation
IEEE Access
Attitude error
coordinate transformation
error compensation
Kalman filtering
Steadicam head
title Development of Steady Aiming System Based on Kalman Filter and Coordinate Transformation
title_full Development of Steady Aiming System Based on Kalman Filter and Coordinate Transformation
title_fullStr Development of Steady Aiming System Based on Kalman Filter and Coordinate Transformation
title_full_unstemmed Development of Steady Aiming System Based on Kalman Filter and Coordinate Transformation
title_short Development of Steady Aiming System Based on Kalman Filter and Coordinate Transformation
title_sort development of steady aiming system based on kalman filter and coordinate transformation
topic Attitude error
coordinate transformation
error compensation
Kalman filtering
Steadicam head
url https://ieeexplore.ieee.org/document/10160027/
work_keys_str_mv AT yufanglu developmentofsteadyaimingsystembasedonkalmanfilterandcoordinatetransformation
AT lishameng developmentofsteadyaimingsystembasedonkalmanfilterandcoordinatetransformation
AT haihuatang developmentofsteadyaimingsystembasedonkalmanfilterandcoordinatetransformation
AT leishi developmentofsteadyaimingsystembasedonkalmanfilterandcoordinatetransformation