In this article, an algorithm for identifying the thrust force and the coefficients of the aerodynamic drag of the aircraft according to the data of the flight experiment is proposed. In order to ensure identifiability, a special flight maneuver is considered. To reduce the impact of measurement noise, the maximum likelihood estimation is used. The results of the study of the algorithm characteristics based on the flight simulation data are presented.
Identification of the Engine Thrust Force Using Flight Test Data
Lect. Notes Electrical Eng.
International Conference on Aerospace System Science and Engineering ; 2021 July 14, 2021 - July 16, 2021
Proceedings of the International Conference on Aerospace System Science and Engineering 2021 ; Kapitel : 30 ; 403-408
2022-07-09
6 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Propulsion , Engine thrust , Identification , Flight tests , Flight dynamics , Aerodynamic drag Engineering , Aerospace Technology and Astronautics , Communications Engineering, Networks , Space Sciences (including Extraterrestrial Physics, Space Exploration and Astronautics) , Control and Systems Theory
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