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  Investigation into Pilot Perception and Control During Decrab Maneuvers in Simulated Flight

Beukers, J., Stroosma O, Pool, D., Mulder, M., & van Paassen, M. (2010). Investigation into Pilot Perception and Control During Decrab Maneuvers in Simulated Flight. Journal of Guidance, Control, and Dynamics, 33(4), 1048-1063. doi:10.2514/1.47774.

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 Creators:
Beukers, JT, Author
Stroosma O, Pool, DM1, Author           
Mulder, M, Author
van Paassen, MM, Author
Affiliations:
1Department Human Perception, Cognition and Action, Max Planck Institute for Biological Cybernetics, Max Planck Society, ou_1497797              

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 Abstract: Anexperiment was conducted in theSIMONAResearch Simulator at Delft University of Technology to investigate the influence of sway, roll, and yaw motion cues on pilot performance, control, and motion perception during decrab maneuvers. In the experiment, six pilots were instructed to perform manual decrab maneuvers in heavy crosswind conditions with a Cessna Citation 500 model. The contributions of yaw, roll, and sway motion stimuli were varied such that their effects on objective measures and subjective ratings could be examined. The results of this experiment show that yaw motion had a positive influence on performance in terms of lateral touchdown distance from the runway centerline. Roll motion significantly decreased roll rate variations during decrab. High workload and the relatively low intensity of lateral motion cues led to the fact that pilots were unable to give consistent fidelity ratings. This result emphasizes the need for an objective and quantifiable method to determine motion fidelity for such maneuvers. Pilot models can possibly be used to further investigate the influence of different motion cues in these transient control tasks.

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 Dates: 2010-08
 Publication Status: Issued
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 Identifiers: URI: http://www1.aiaa.org/content.cfm?pageid=406gTable=jaPapergid=47774
DOI: 10.2514/1.47774
BibTex Citekey: BeukersSPMV2010
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Title: Journal of Guidance, Control, and Dynamics
Source Genre: Journal
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Pages: - Volume / Issue: 33 (4) Sequence Number: - Start / End Page: 1048 - 1063 Identifier: -