Flying qualities and flight control system design for a fly-by-wire transport aircraft

Fly-by-wire flight control systems are becoming more common in both civil and military aircraft. These systems give many benefits, but also present a new set of problems due to their increased complexity compared to conventional systems and the larger choice of options that they provide. The work pr...

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Bibliographic Details
Main Author: Gautrey, Jim
Other Authors: Cook, M. V.
Language:en
Published: Cranfield University 2015
Subjects:
Online Access:http://dspace.lib.cranfield.ac.uk/handle/1826/9594
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spelling ndltd-CRANFIELD1-oai-dspace.lib.cranfield.ac.uk-1826-95942015-11-24T03:24:30ZFlying qualities and flight control system design for a fly-by-wire transport aircraftGautrey, Jimfly-by-wireFly-by-wire flight control systems are becoming more common in both civil and military aircraft. These systems give many benefits, but also present a new set of problems due to their increased complexity compared to conventional systems and the larger choice of options that they provide. The work presented here considers the application of fly-by-wire to a generic regional transport aircraft. The flying qualities criteria used for typical flying qualities evaluations are described briefly followed by analysis of several past transport aircraft flying qualities programmes against these criteria. From these results, some control law independent design requirements are formulated for a civil aircraft for the approach and landing task. These control law independent flying qualities criteria are intended to be used with any generic rate-like control law for a transport aircraft and enabled a number of different control laws to be designed. The results of a number of flying qualities evaluations are presented. Both an ILS approach task and a formation flying task were used. The effects of windshear were also considered. It was found that control laws which maintain flight path are suitable for the ILS approach task, while most rate-like response characteristics give good flying qualities for the formation flying task. Finally, the conclusions drawn from these evaluations are presented, and both the Civil and Military current airworthiness requirements are assessed. In addition to the flying qualities work, a study is made of the management issues associated with fly-by-wire design. A fly-by-wire aircraft design programme was proposed and the project management issues associated with this were considered. A timescale was proposed for the design process for a generic regional aircraft, and the critical path for this process is presented.EPSRC; Avro International Aerospace.Cranfield UniversityCollege of Aeronautics (SoE)Cook, M. V.2015-11-23T10:44:03Z2015-11-23T10:44:03Z1998-09Thesis or dissertationDoctoralEngDhttp://dspace.lib.cranfield.ac.uk/handle/1826/9594enThis thesis is submitted in partial fulfilment of the requirements for the Degree of Doctor of Engineering.
collection NDLTD
language en
sources NDLTD
topic fly-by-wire
spellingShingle fly-by-wire
Gautrey, Jim
Flying qualities and flight control system design for a fly-by-wire transport aircraft
description Fly-by-wire flight control systems are becoming more common in both civil and military aircraft. These systems give many benefits, but also present a new set of problems due to their increased complexity compared to conventional systems and the larger choice of options that they provide. The work presented here considers the application of fly-by-wire to a generic regional transport aircraft. The flying qualities criteria used for typical flying qualities evaluations are described briefly followed by analysis of several past transport aircraft flying qualities programmes against these criteria. From these results, some control law independent design requirements are formulated for a civil aircraft for the approach and landing task. These control law independent flying qualities criteria are intended to be used with any generic rate-like control law for a transport aircraft and enabled a number of different control laws to be designed. The results of a number of flying qualities evaluations are presented. Both an ILS approach task and a formation flying task were used. The effects of windshear were also considered. It was found that control laws which maintain flight path are suitable for the ILS approach task, while most rate-like response characteristics give good flying qualities for the formation flying task. Finally, the conclusions drawn from these evaluations are presented, and both the Civil and Military current airworthiness requirements are assessed. In addition to the flying qualities work, a study is made of the management issues associated with fly-by-wire design. A fly-by-wire aircraft design programme was proposed and the project management issues associated with this were considered. A timescale was proposed for the design process for a generic regional aircraft, and the critical path for this process is presented. === EPSRC; Avro International Aerospace.
author2 Cook, M. V.
author_facet Cook, M. V.
Gautrey, Jim
author Gautrey, Jim
author_sort Gautrey, Jim
title Flying qualities and flight control system design for a fly-by-wire transport aircraft
title_short Flying qualities and flight control system design for a fly-by-wire transport aircraft
title_full Flying qualities and flight control system design for a fly-by-wire transport aircraft
title_fullStr Flying qualities and flight control system design for a fly-by-wire transport aircraft
title_full_unstemmed Flying qualities and flight control system design for a fly-by-wire transport aircraft
title_sort flying qualities and flight control system design for a fly-by-wire transport aircraft
publisher Cranfield University
publishDate 2015
url http://dspace.lib.cranfield.ac.uk/handle/1826/9594
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