Please use this identifier to cite or link to this item: https://hdl.handle.net/20.500.13087/900
Title: Pitch-Rate Control Augmentation System Design for Delayed Measurements
Authors: Gümüşboğa, İlkay
İftar, Altuğ
Issue Date: 2019
Publisher: IEEE
Abstract: The pitch-rate control augmentation system is important especially for the military aerospace industry. In this study, it is shown that the classical control structure in the literature cannot cope with the time-delays that may occur in the measurements and a new control structure, based on a modified Smith predictor, is proposed. This proposed structure is verified by nonlinear flight simulations, where all dynamics of the F-16 aircraft are taken into account, including the nonlinearities in the elevator dynamics. With these nonlinear flight simulations, which are undertaken under a realistic scenario, it is shown that the proposed control system can cope with the time-delays and can successfully track pitch-rate commands.
Description: 6th International Conference on Control, Decision and Information Technologies (CoDIT) -- APR 23-26, 2019 -- Conservatoire Nat Arts Metiers, Paris, FRANCE
URI: https://hdl.handle.net/20.500.13087/900
ISBN: 978-1-7281-0521-5
ISSN: 2576-3555
Appears in Collections:Scopus İndeksli Yayınlar Koleksiyonu
WoS İndeksli Yayınlar Koleksiyonu
Çevre Mühendisliği Bölümü Koleksiyonu

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