CUED Publications database

Vibration suppression in flight control with dynamic inversion

Papageorgiou, C and Glover, K (2002) Vibration suppression in flight control with dynamic inversion. In: UNSPECIFIED pp. 223-228..

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Abstract

Copyright © 2002 IFAC. Classical flight control design techniques treat the aircrafts as rigid bodies. Extra effort and time is required for the development of a separate vibration controller that addresses the flexible nature of the aircraft. Researchers have concentrated in developing integrated design techniques where a single controller is designed to provide satisfactory control of the rigid modes, and vibration suppression of the structural modes. This paper presents the application of such an integrated design procedure for the pitch rate control of a twin-fin combat aircraft. The proposed technique is easy to apply and generates a simple, low-order controller that satisfies the design objectives.

Item Type: Conference or Workshop Item (UNSPECIFIED)
Subjects: UNSPECIFIED
Divisions: Div F > Control
Depositing User: Cron Job
Date Deposited: 17 Jul 2017 19:32
Last Modified: 24 Oct 2019 14:14
DOI: