Cockpit integration from a pilot's point of viewExtensive experience in both operational and engineering test flight was used to suggest straightforward changes to helicopter cockpit and control system design that would improve pilot performance in marginal and instrument flight conditions. Needed control system improvements considered include: (1) separation of yaw from cyclic force trim; (2) pedal force proportional to displacement rate; and (3) integration of engine controls in collective stick. Display improvements needed include: (1) natural cuing of yaw rate in attitude indicator; (2) collective position indication and radar altimeter placed within primary scan; and (3) omnidirectional display of full range airspeed data.
Document ID
19820015350
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Green, D. L. (Pacer Systems, Inc. Arlington, VA, United States)
Date Acquired
August 10, 2013
Publication Date
April 1, 1982
Publication Information
Publication: NASA. Ames Research Center Helicopter Handling Qualities