Fixed Wing Aircraft Linear Velocity Estimation using a Reduced order Observer

In this paper we propose a reduced observer design for aircraft linear velocity estimation based on the measurements of the Euler angles and angular velocity as well as the position which is subject to measurement errors and noise. The observer is designed based on a high gain approach using an outp...

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Bibliographic Details
Published in2019 International Conference on Advanced Electrical Engineering (ICAEE) pp. 1 - 6
Main Authors Hamissi, A., Bouzid, Y., Zaouche, M., Malko, L., Hamerain, M., Busawon, K.
Format Conference Proceeding
LanguageEnglish
Published IEEE 01.11.2019
Subjects
Aircraft
Aircraft linear velocity estimation
Aircraft propulsion
Atmospheric modeling
Global Positioning System
high gain observer
Jetstream-3102
MFS2004
Noise measurement
Observers
utput injection
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Summary:In this paper we propose a reduced observer design for aircraft linear velocity estimation based on the measurements of the Euler angles and angular velocity as well as the position which is subject to measurement errors and noise. The observer is designed based on a high gain approach using an output injection, which enables to reduce the order of the observer to six equations rather than a full order observer of order 12. To show the performance of the observer as well as its robustness with respect to measurement errors and noise, a simulation study is carried out using a British aircraft Jetstream-3102 in a real-time virtual simulation platform base on Microsoft Flight Simulator (FS-2004).
DOI:10.1109/ICAEE47123.2019.9015073