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Ground-Based Simulation of Airplane ...

University of Toronto (Canada).

Ground-Based Simulation of Airplane Upset Using an Enhanced Flight Model.

紀錄類型:	書目-語言資料,印刷品 : Monograph/item
正題名/作者:	Ground-Based Simulation of Airplane Upset Using an Enhanced Flight Model./
作者:	Liu, Stacey Fangfei.
面頁冊數:	99 p.
附註:	Source: Masters Abstracts International, Volume: 50-03, page: 1829.
Contained By:	Masters Abstracts International50-03.
標題:	Engineering, Aerospace. -
電子資源:	http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=MR76094
ISBN:	9780494760949

Ground-Based Simulation of Airplane Upset Using an Enhanced Flight Model.
Liu, Stacey Fangfei.

Ground-Based Simulation of Airplane Upset Using an Enhanced Flight Model. - 99 p.

Source: Masters Abstracts International, Volume: 50-03, page: 1829.

Thesis (M.A.Sc.)--University of Toronto (Canada), 2011.

Loss-of-control resulting from airplane upset is a leading cause of worldwide commercial aircraft accidents. One of the upset prevention and recovery strategies currently being considered is to provide pilot upset recovery training using ground-based flight simulators. However, to simulate the large amplitude and highly dynamic motions seen in upset conditions, both the flight model and the simulator motion need improvement.

ISBN: 9780494760949Subjects--Topical Terms:

845476
Engineering, Aerospace.

Ground-Based Simulation of Airplane Upset Using an Enhanced Flight Model.
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100 1 $a Liu, Stacey Fangfei. $3 845685
245 1 0 $a Ground-Based Simulation of Airplane Upset Using an Enhanced Flight Model.
300 $a 99 p.
500 $a Source: Masters Abstracts International, Volume: 50-03, page: 1829.
500 $a Adviser: Peter R. Grant.
502 $a Thesis (M.A.Sc.)--University of Toronto (Canada), 2011.
520 $a Loss-of-control resulting from airplane upset is a leading cause of worldwide commercial aircraft accidents. One of the upset prevention and recovery strategies currently being considered is to provide pilot upset recovery training using ground-based flight simulators. However, to simulate the large amplitude and highly dynamic motions seen in upset conditions, both the flight model and the simulator motion need improvement.
520 $a In this thesis, an enhanced flight model is developed to better represent the aircraft dynamics in upset conditions. In particular, extension is made to the aerodynamic database of an existing Boeing 747-100 (B-747) model to cover large angle of attack, sideslip and angular rates. The enhanced B-747 model is then used to conduct a set of upset recovery experiments in a flight simulator without motion. The experimental results can be used to identify and potentially correct major motion cueing errors caused by the conventional motion drive algorithm in upset conditions.
590 $a School code: 0779.
650 4 $a Engineering, Aerospace. $3 845476
690 $a 0538
710 2 $a University of Toronto (Canada). $b Aerospace Science and Engineering. $3 845686
773 0 $t Masters Abstracts International $g 50-03.
790 1 0 $a Grant, Peter R., $e advisor
790 $a 0779
791 $a M.A.Sc.
792 $a 2011
856 4 0 $u http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=MR76094

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