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US-German Joint In-flight and Simulator Evaluation of Collective Tactile Cueing for Torque Limit Avoidance: Shaker versus Soft Stop

Müllhäuser, Mario Rene and Lusardi, Jeff A. (2022) US-German Joint In-flight and Simulator Evaluation of Collective Tactile Cueing for Torque Limit Avoidance: Shaker versus Soft Stop. Journal of the American Helicopter Society, 67 (3), pp. 69-84. American Helicopter Society. doi: 10.4050/JAHS.67.032006. ISSN 0002-8711.

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Official URL: https://www.ingentaconnect.com/content/10.4050/JAHS.67.032006

Abstract

The demonstration and testing of tactile cueing was the subject of a common research undertaking by the U.S. Army Combat Capabilities Development Command Aviation & Missile Center and the German Aerospace Center. The primary objective was to test a torque protection system with both a stick shaking cue generated with an attachable stick shaker and a soft stop cue generated by an active inceptor system. It was tested by five pilots in flight on the RASCAL JUH-60A helicopter and by four pilots in the ground-based simulator of the ACT/FHS (H-135) research helicopter based on a common set of high-performance takeoff mission profiles. The qualitative evaluation showed that the soft stop provided a greater workload reduction than the shaker and was the preferred cue. However, a shaker cue is a promising alternative when the application of an active inceptor system is not possible.

Item URL in elib:https://elib.dlr.de/187544/
Document Type:Article
Title:US-German Joint In-flight and Simulator Evaluation of Collective Tactile Cueing for Torque Limit Avoidance: Shaker versus Soft Stop
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Müllhäuser, Mario ReneUNSPECIFIEDhttps://orcid.org/0000-0003-3721-4881UNSPECIFIED
Lusardi, Jeff A.US Army CCDCUNSPECIFIEDUNSPECIFIED
Date:28 January 2022
Journal or Publication Title:Journal of the American Helicopter Society
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:67
DOI:10.4050/JAHS.67.032006
Page Range:pp. 69-84
Publisher:American Helicopter Society
ISSN:0002-8711
Status:Published
Keywords:Active Sidestick, Active Inceptor, Aktive Steuerorgane, tactile Cueing, Flight Test, Limit Protection, Limit Avoidance, Flugerprobung
HGF - Research field:other
HGF - Program:other
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L DT - Defense Technology
DLR - Research theme (Project):L - Support
Location: Braunschweig
Institutes and Institutions:Institute of Flight Systems > Rotorcraft
Institute of Flight Systems
Deposited By: Müllhäuser, Mario Rene
Deposited On:29 Nov 2022 16:18
Last Modified:19 Oct 2023 13:51

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