Development of a pilot model suitable for the simulation of large aircraft

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dc.contributor.authorLone, Mohammad M.
dc.contributor.authorCooke, Alastair K.
dc.date.accessioned2017-06-20T15:11:01Z
dc.date.available2017-06-20T15:11:01Z
dc.date.issued2010-09
dc.description.abstractEffects of aeroservoelasticity on the manual control of large civil aircraft are investigated through a pilot modelling approach based on the modified optimal control model. A synopsis of modelling techniques is presented, followed by the description of the adopted technique. A simulation environment suitable for investigating pilot-vehicle dynamics in the longitudinal axis has been developed. The derivation of the pilot model was based on limiting the bandwidth. This approach showed that the pilot-vehicle system satisfied the crossover law between 3rad/s to 10rad/s for normal acceleration response. It was found that the pilot model and the low frequency tailplane bending mode introduced a resonant peak in the pilotvehicle frequency response that may be a cause for concern in high gain scenarios. Gust response simulations highlighted the contribution of fuselage bending mode on pilot perceived normal acceleration.en_UK
dc.identifier.citationLone MM, Cooke AK. (2010) Development of a pilot model suitable for the simulation of large aircraft. Proceedings of the 27th congress of the International Council of the Aeronautical Sciences (ICAS 2010), 19-24th September 2010, Nice, Franceen_UK
dc.identifier.isbn9781617820496
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/12073
dc.language.isoenen_UK
dc.publisherOptimage Ltd. on behalf of the International Council of the Aeronautical Sciencesen_UK
dc.rights©2010 ICAS. This is the Author Accepted Manuscript. Please refer to any applicable publisher terms of use.
dc.subjectpilot modellingen_UK
dc.subjectlarge aircraften_UK
dc.subjectaeroservoelasticityen_UK
dc.titleDevelopment of a pilot model suitable for the simulation of large aircraften_UK
dc.typeConference paperen_UK

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