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Simple control law structure for the control of airplanes by means of their engines

Fezans, Nicolas (2011) Simple control law structure for the control of airplanes by means of their engines. In: Selected Papers of the 1st CEAS Specialist Conference on Guidance, Navigation and Control, pp. 151-162. Springer-Verlag Berlin Heidelberg. CEAS EuroGNC Conference, 13.-15. April 2011, München. ISBN 973 3 642 19816 8.

Full text not available from this repository.

Abstract

In this paper a simple control law structure is presented for the control of airplanes using only the engines' thrust. For the design of such a propulsion controlled aircraft control law, the approach followed in this work is to look for the right level of performance in order to avoid both excessive engines activity and reduction of robustness properties. Another goal is to keep the control law and its tuning as simple as possible: for this a control law structure whose terms can easily be interpreted is proposed. The capability of the proposed control law to permit safe landing was shown by simulator tests as well as flight tests.

Document Type:Conference or Workshop Item (Paper)
Title:Simple control law structure for the control of airplanes by means of their engines
Authors:
AuthorsInstitution or Email of Authors
Fezans, Nicolasnicolas.fezans@dlr.de
Date:February 2011
Journal or Publication Title:Selected Papers of the 1st CEAS Specialist Conference on Guidance, Navigation and Control
Page Range:pp. 151-162
Editors:
EditorsEmail
Holzapfel, Florianflorian.holzapfel@tum.de
Theil, Stephanstephan.theil@dlr.de
Publisher:Springer-Verlag Berlin Heidelberg
Series Name:Advances in Aerospace Guidance, Navigation and Control
ISBN:973 3 642 19816 8
Status:Published
Keywords:propulsion-controlled aircraft, flight control law, flight test, ATTAS
Event Title:CEAS EuroGNC Conference
Event Location:München
Event Type:international Conference
Event Dates:13.-15. April 2011
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Systems & Cabin
Location: Braunschweig
Institutes and Institutions:Institute of Flight Systems > Flight Dynamics and Simulation
Deposited By: Nicolas Fezans
Deposited On:17 May 2011 13:19
Last Modified:17 May 2011 13:19

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