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  Identification of Pilot Control Behavior in a Roll-Lateral Helicopter Hover Task

Nieuwenhuizen, F., Beykirch, K., Mulder, M., & Bülthoff, H. (2007). Identification of Pilot Control Behavior in a Roll-Lateral Helicopter Hover Task. In AIAA Modeling and Simulation Technologies Conference and Exhibit 2007 (pp. 975-985). Reston, VA, USA: American Institute of Aeronautics and Astronautics.

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Basisdaten

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Datensatz-Permalink: https://hdl.handle.net/11858/00-001M-0000-0013-CC41-2 Versions-Permalink: https://hdl.handle.net/21.11116/0000-0003-D810-7
Genre: Konferenzbeitrag

Externe Referenzen

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externe Referenz:
https://arc.aiaa.org/doi/10.2514/6.2007-6799 (Verlagsversion)
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Urheber

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 Urheber:
Nieuwenhuizen, FM1, 2, Autor           
Beykirch, K1, 2, Autor           
Mulder, M, Autor
Bülthoff, HH1, 2, Autor           
Affiliations:
1Department Human Perception, Cognition and Action, Max Planck Institute for Biological Cybernetics, Max Planck Society, ou_1497797              
2Max Planck Institute for Biological Cybernetics, Max Planck Society, Spemannstrasse 38, 72076 Tübingen, DE, ou_1497794              

Inhalt

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Schlagwörter: -
 Zusammenfassung: This paper focuses on the influence of different forms of motion feedback on the per-
ception and control behavior of pilots in a roll-lateral helicopter hover task. To identify
this influence, a combined target-following and disturbance-rejection task is carried out
where the motion feedback is varied. The participants perform the control task with roll
motion only, lateral motion only, combined roll-lateral motion, or with no motion. A cy-
bernetic approach is taken to identify multi-loop pilot describing functions and estimate
the parameters of a pilot model. Results show that participants perform significantly bet-
ter at the control task with feedback of combined roll-lateral motion, and decrease their
control activity. For the condition with feedback of roll motion a similar trend is observed.
This is explained through the increased amount of information present in the inner roll
stabilization loop.

Details

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Sprache(n):
 Datum: 2007-08
 Publikationsstatus: Erschienen
 Seiten: -
 Ort, Verlag, Ausgabe: -
 Inhaltsverzeichnis: -
 Art der Begutachtung: -
 Identifikatoren: DOI: 10.2514/6.2007-6799
BibTex Citekey: 4660
 Art des Abschluß: -

Veranstaltung

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Titel: AIAA Modeling and Simulation Technologies Conference and Exhibit 2007
Veranstaltungsort: Hilton Head, SC, USA
Start-/Enddatum: 2007-08-20 - 2007-08-23

Entscheidung

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Projektinformation

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Quelle 1

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Titel: AIAA Modeling and Simulation Technologies Conference and Exhibit 2007
Genre der Quelle: Konferenzband
 Urheber:
Affiliations:
Ort, Verlag, Ausgabe: Reston, VA, USA : American Institute of Aeronautics and Astronautics
Seiten: - Band / Heft: - Artikelnummer: - Start- / Endseite: 975 - 985 Identifikator: ISBN: 978-1-62410-160-1