Design and evaluation of the objective motion cueing test and criterion

Author:

Hosman R.,Advani S.

Abstract

ABSTRACTSince the introduction of hexapod-type motion systems for flight simulation in the 1970s, Motion Drive Algorithm tuning has been primarily based on the subjective judgement of experienced pilots. This subjective method is often not transparent and often leads to ambiguous process of adjustment of the tuning parameters. Consequently, there are large variations in the motion cueing characteristics of flight training devices, a variability that subsequently raises questions regarding the value of motion cueing for pilot training itself. The third revision of ICAO 9625 Manual of Criteria for the Qualification of Flight Simulation Training Devices offered the opportunity to take a closer look at simulator motion cueing requirements in general. This led to the concept of the objective motion cueing test (OMCT), which was reported in 2006. After the method was evaluated on three research flight simulators, the results were published in 2007, demonstrating a larger spread in dynamic behaviour of cueing algorithms than expected. After discussions with the simulator industry regarding the form and methodology of the OMCT, an evaluation of the test in cooperation with the industry started in 2011. This led to the final form of the OMCT and cueing parameter criterion for the in-flight mode of transport aircraft. This paper describes the OMCT, the evaluation results and the criterion.

Publisher

Cambridge University Press (CUP)

Subject

Aerospace Engineering

Reference31 articles.

1. Anon . FAA Part 60. Flight Simulation Training Device Initial and Continuing Qualification and Use. 2008.

2. Reid L.D. and Nahon M.A. Flight simulation motion-base drive algorithms: Part 2 – selecting the system parameters, 1985, Institute of Aerospace Studies, University of Toronto. UTIAS Report 307.

3. Parrish R.V. , Dieudonne J.E. and Martin D.J. Motion Software for a Synergistic Six-Degree-of-Freedom Motion Base. NASA TN D-7350. Washington: NASA, 1973.

4. Anon . Airplane Simulator and Visual System Evaluation. FAA Advisory Circular AC 120-40A, 1986.

5. Stapleford R.L. , Peters R.A. and Alex F.R. Experiments and a model for pilot dynamics with visual and motion inputs. 1969, NASA CR-1325.

Cited by 22 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3