Acceptance testing and commissioning of a flight simulator for rotorcraft simulation fidelity research

被引:28
|
作者
White, Mark D. [1 ,2 ]
Perfect, Philip [1 ,2 ]
Padfield, Gareth D. [1 ,2 ]
Gubbels, Arthur W. [3 ]
Berryman, Andrew C.
机构
[1] Univ Liverpool, Ctr Engn Dynam, Liverpool L69 7ZB, Merseyside, England
[2] Univ Liverpool, Sch Engn, Liverpool L69 7ZB, Merseyside, England
[3] CNR, Flight Res Lab, Ottawa, ON, Canada
基金
英国工程与自然科学研究理事会;
关键词
Flight; simulator; rotorcraft; fidelity; HANDLING QUALITIES;
D O I
10.1177/0954410012439816
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The rotorcraft industry faces a number of challenges today regarding the replacement of ageing airframes, an expansion in the operational roles of helicopters and a requirement to improve safety whilst reducing the environmental impact of rotorcraft operations. The quantification of simulation fidelity underpins the confidence required for the expanding use of modelling and simulation to develop solutions to these challenges in a timely and cost-efficient manner. Current simulator certification standards do not provide a fully quantitative method for assessing simulation fidelity, especially in a research environment. This article details the commissioning and acceptance process of the new research flight simulation facility at the University of Liverpool, HELIFLIGHT-R, and its subsequent use in a research project 'Lifting Standards: A Novel Approach to the Development of Fidelity Criteria for Rotorcraft Flight Simulators' aimed at developing new predicted and perceptual measures of simulator fidelity. Some initial results from both piloted simulation and flight tests using the Bell 412 Advanced Systems Research Aircraft are reported within the context of the rotorcraft simulation fidelity project.
引用
收藏
页码:663 / 686
页数:24
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