Design and evaluation of a Flight Envelope Protection haptic feedback system

Joost Ellerbroek; Mitchell Rodriguez Martin; T Lombaerts; Rene van Paassen; Max Mulder

doi:10.1016/j.ifacol.2016.10.481

Design and evaluation of a Flight Envelope Protection haptic feedback system

Joost Ellerbroek, Mitchell Rodriguez Martin, T Lombaerts, Rene van Paassen, Max Mulder

Research output: Contribution to journal › Conference article › Scientific › peer-review

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Abstract

This paper describes the design and evaluation of a shared control, haptic feedback system to communicate Flight Envelope Protection System intent. The concept uses a combination of stiffness feedback and vibration to communicate proximity of the aircraft state to flight envelope boundaries. In addition, a stick center shift can be applied by the envelope protection system to cooperatively perform corrective actions in case of severe excursions of the envelope margins. Results from the evaluation experiment show improved performance with haptic feedback in both scenarios. Workload ratings were unaffected. Pilot opinion was unanimously positive, especially with regard to the combination of stiffness feedback and vibration cues.

Original language	English
Pages (from-to)	171-176
Journal	IFAC-PapersOnLine
Volume	49
Issue number	19
DOIs	https://doi.org/10.1016/j.ifacol.2016.10.481
Publication status	Published - 2016
Event	13th IFAC Symposium on Analysis, Design, and Evaluation of Human-Machine Systems - Kyoto, Japan Duration: 30 Aug 2016 → 2 Sep 2016

Keywords

shared control
haptics
flight envelope protection

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10.1016/j.ifacol.2016.10.481

IFAC2016_EllerbroekAccepted author manuscript, 204 KBLicence: CC BY-NC-ND

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title = "Design and evaluation of a Flight Envelope Protection haptic feedback system",

abstract = "This paper describes the design and evaluation of a shared control, haptic feedback system to communicate Flight Envelope Protection System intent. The concept uses a combination of stiffness feedback and vibration to communicate proximity of the aircraft state to flight envelope boundaries. In addition, a stick center shift can be applied by the envelope protection system to cooperatively perform corrective actions in case of severe excursions of the envelope margins. Results from the evaluation experiment show improved performance with haptic feedback in both scenarios. Workload ratings were unaffected. Pilot opinion was unanimously positive, especially with regard to the combination of stiffness feedback and vibration cues.",

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AU - Ellerbroek, Joost

AU - Rodriguez Martin, Mitchell

AU - Lombaerts, T

AU - van Paassen, Rene

AU - Mulder, Max

PY - 2016

Y1 - 2016

N2 - This paper describes the design and evaluation of a shared control, haptic feedback system to communicate Flight Envelope Protection System intent. The concept uses a combination of stiffness feedback and vibration to communicate proximity of the aircraft state to flight envelope boundaries. In addition, a stick center shift can be applied by the envelope protection system to cooperatively perform corrective actions in case of severe excursions of the envelope margins. Results from the evaluation experiment show improved performance with haptic feedback in both scenarios. Workload ratings were unaffected. Pilot opinion was unanimously positive, especially with regard to the combination of stiffness feedback and vibration cues.

AB - This paper describes the design and evaluation of a shared control, haptic feedback system to communicate Flight Envelope Protection System intent. The concept uses a combination of stiffness feedback and vibration to communicate proximity of the aircraft state to flight envelope boundaries. In addition, a stick center shift can be applied by the envelope protection system to cooperatively perform corrective actions in case of severe excursions of the envelope margins. Results from the evaluation experiment show improved performance with haptic feedback in both scenarios. Workload ratings were unaffected. Pilot opinion was unanimously positive, especially with regard to the combination of stiffness feedback and vibration cues.

KW - shared control

KW - haptics

KW - flight envelope protection

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DO - 10.1016/j.ifacol.2016.10.481

M3 - Conference article

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SP - 171

EP - 176

JO - IFAC-PapersOnLine

JF - IFAC-PapersOnLine

SN - 1474-6670

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T2 - 13th IFAC Symposium on Analysis, Design, and Evaluation of Human-Machine Systems

Y2 - 30 August 2016 through 2 September 2016

ER -

Design and evaluation of a Flight Envelope Protection haptic feedback system

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