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Model analysis of remotely controlled rendezvous and docking with display predictionManual control of rendezvous and docking (RVD) of two spacecraft in low earth orbit by a remote human operator is discussed. Experimental evidence has shown that control performance degradation for large transmission delays (between spacecraft and operations control center) can be substantially improved by the introduction of predictor displays. An intial Optimal Control Model (OCM) analysis of RVD translational and rotational perturbation control was performed, with emphasis placed on the predictive capabilities of the combined Kalman estimator/optimal predictor with respect to control performance, for a range of time delays, motor noise levels and tracking axes. OCM predictions are then used as a reference for comparing tracking performance with a simple predictor display, as well as with no display prediction at all. Use is made here of an imperfect internal model formulation, whereby it is assumed that the human operator has no knowledge of the system transmission delay.
Document ID
19860023531
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Milgram, P.
(National Aerospace Lab. Amsterdam, Netherlands)
Wewerinke, P. H.
(National Aerospace Lab. Amsterdam, Netherlands)
Date Acquired
August 12, 2013
Publication Date
May 1, 1986
Publication Information
Publication: NASA. Ames Research Center, 21st Annual Conference on Manual Control
Subject Category
Man/System Technology And Life Support
Accession Number
86N33003
Funding Number(s)
CONTRACT_GRANT: ESA-5594/83/NL/AN(SC)
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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