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An attitude estimate method for fixed-wing UAV s using MEMS/GPS data fusion

  • Beihang University

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

Unmanned Aerial Vehicles(UAVs) require high performance Attitude and Heading Reference System(AHRS) in automatic flight. This paper presents an attitude estimate method using Micro Electro Mechanical Systems(MEMS) and GPS data fusions. An Extended Kalman Filter(EKF) is developed in the algorithm. The measurements of MEMS Inertial Measuring Units(IMUs) and GPS receiver are modeled. The observation equations of EKF are simplified by the augmentation of GPS-derived accelerations and accelerometer measurements, which can reduce computational overhead. Simulation tests show the effectiveness of the proposed attitude estimate method.

源语言英语
主期刊名1st International Conference on Electronics Instrumentation and Information Systems, EIIS 2017
编辑Jun-Bao Li
出版商Institute of Electrical and Electronics Engineers Inc.
1-5
页数5
ISBN(电子版)9781538608432
DOI
出版状态已出版 - 2 7月 2017
活动1st International Conference on Electronics Instrumentation and Information Systems, EIIS 2017 - Harbin, 中国
期限: 3 6月 20175 6月 2017

出版系列

姓名1st International Conference on Electronics Instrumentation and Information Systems, EIIS 2017
2018-January

会议

会议1st International Conference on Electronics Instrumentation and Information Systems, EIIS 2017
国家/地区中国
Harbin
时期3/06/175/06/17

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