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Motion Cueing Algorithm Development: Human-Centered Linear and Nonlinear ApproachesWhile the performance of flight simulator motion system hardware has advanced substantially, the development of the motion cueing algorithm, the software that transforms simulated aircraft dynamics into realizable motion commands, has not kept pace. Prior research identified viable features from two algorithms: the nonlinear "adaptive algorithm", and the "optimal algorithm" that incorporates human vestibular models. A novel approach to motion cueing, the "nonlinear algorithm" is introduced that combines features from both approaches. This algorithm is formulated by optimal control, and incorporates a new integrated perception model that includes both visual and vestibular sensation and the interaction between the stimuli. Using a time-varying control law, the matrix Riccati equation is updated in real time by a neurocomputing approach. Preliminary pilot testing resulted in the optimal algorithm incorporating a new otolith model, producing improved motion cues. The nonlinear algorithm vertical mode produced a motion cue with a time-varying washout, sustaining small cues for longer durations and washing out large cues more quickly compared to the optimal algorithm. The inclusion of the integrated perception model improved the responses to longitudinal and lateral cues. False cues observed with the NASA adaptive algorithm were absent. The neurocomputing approach was crucial in that the number of presentations of an input vector could be reduced to meet the real time requirement without degrading the quality of the motion cues.
Document ID
20050180246
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Houck, Jacob A.
(NASA Langley Research Center Hampton, VA, United States)
Telban, Robert J.
(State Univ. of New York Binghamton, NY, United States)
Cardullo, Frank M.
(State Univ. of New York Binghamton, NY, United States)
Date Acquired
September 7, 2013
Publication Date
May 1, 2005
Subject Category
Numerical Analysis
Report/Patent Number
NASA/CR-2005-213747
Funding Number(s)
WORK_UNIT: WU 23-090-70-10
CONTRACT_GRANT: NASA Order L-70823-D
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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