NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Quantification of Cross-coupling and Motion Feedthrough for Multiaxis Controllers Used in an Air Combat Flying TaskA real-time piloted simulation of an air-to-air combat flying task using a wings-level-turn aircraft and various novel controllers was conducted. One objective is to quantify how the pilot interacts with the controllers and control modes, including: (1) controller versus aircraft response; (2) proprioceptive cross-coupling among axes of the controllers; and (3) biodynamic cross-coupling between the aircraft motions and the controllers. In order to aid in identifying the items listed above, both the target aircraft and the large amplitude multimode aerospace research simulator (LAMARS) motion system were distributed with quasi-random sums-of-sinusoids. Since the disturbances were separated in frequency, spectral analysis techniques were used to identify the three items listed. The results of the spectral analysis of controller motions from the two-axis side stick, a twist grip mounted on the side stick, a thumb button mounted on the side stick, and conventional rudder pedals are presented. Conclusions and recommendations for further research are also presented.
Document ID
19850006182
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jewell, W. E.
(Systems Technology, Inc. Mountain View, CA, United States)
Citurs, K. D.
(McDonnell Aircraft Co. St. Louis, Mo., United States)
Date Acquired
August 12, 2013
Publication Date
September 1, 1984
Publication Information
Publication: NASA. Ames Research Center 20th Ann. Conf. on Manual Control, Vol. 1
Subject Category
Man/System Technology And Life Support
Accession Number
85N14491
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available