Modified attitude factor graph fusion method for unmanned helicopter under atmospheric disturbance

The Unmanned Aerial Helicopter (UAH) has attracted increasing attention in the military and civil areas with the unique flight performance. The significant impact on the attitude measurement performance of UAHs by the strong airflow disturbance is an essential factor threatening flight safety. To im...

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Bibliographic Details
Published inChinese journal of aeronautics Vol. 35; no. 6; pp. 285 - 297
Main Authors SUN, Kecheng, ZENG, Qinghua, LIU, Jianye, QIU, Wenqi, SHI, Jinhen
Format Journal Article
LanguageEnglish
Published Elsevier Ltd 01.06.2022
Jiangsu University Collaborative Innovation Center for Satellite Communication and Navigation,Nanjing 211106,China
Key Laboratory of the MIIT Advanced Aircraft Navigation,Control and Health Management,Nanjing 211106,China
Navigation Research Center,Nanjing University of Aeronautics&Astronautics,Nanjing 211106,China%Navigation Research Center,Nanjing University of Aeronautics&Astronautics,Nanjing 211106,China
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Summary:The Unmanned Aerial Helicopter (UAH) has attracted increasing attention in the military and civil areas with the unique flight performance. The significant impact on the attitude measurement performance of UAHs by the strong airflow disturbance is an essential factor threatening flight safety. To improve the attitude measurement performance of UAHs under atmospheric disturbance, an attitude fusion method over the factor graph is applied and provides the plug-and-play capability. Based on the relationship between position, velocity and attitude, a new attitude correction algorithm for the Modified Attitude Factor Graph Fusion (MAFGF) navigation method is designed and constructed through the fused position and velocity information. Finally, results of simulation and experiment are given to show the effectiveness of the proposed method.
ISSN:1000-9361
DOI:10.1016/j.cja.2021.07.020