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Inertial head-tracker sensor fusion by a complementary separate-bias Kalman filterCurrent virtual environment and teleoperator applications are hampered by the need for an accurate, quick responding head-tracking system with a large working volume. Gyroscopic orientation sensors can overcome problems with jitter, latency, interference, line-of-sight obscurations, and limited range, but suffer from slow drift. Gravimetric inclinometers can detect attitude without drifting, but are slow and sensitive to transverse accelerations. This paper describes the design of a Kalman filter to integrate the data from these two types of sensors in order to achieve the excellent dynamic response of an inertial system without drift, and without the acceleration sensitivity of inclinometers.
Document ID
19960028781
Acquisition Source
Ames Research Center
Document Type
Conference Proceedings
Authors
Foxlin, Eric
(Massachusetts Inst. of Tech. Cambridge, MA United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1996
Publication Information
ISSN: 1087-8270
ISBN: 0-8186-7295-1
Subject Category
Man/System Technology And Life Support
Report/Patent Number
NASA-CR-201055
NAS 1.26:201055
Report Number: NASA-CR-201055
ISBN: 0-8186-7295-1
Report Number: NAS 1.26:201055
ISSN: 1087-8270
Meeting Information
Meeting: IEEE 1996 Virtual Reality Annual International Symposium
Location: Santa Clara, CA
Country: United States
Start Date: March 30, 1996
End Date: April 3, 1996
Accession Number
96N29441
Funding Number(s)
CONTRACT_GRANT: NCC2-771
Distribution Limits
Public
Copyright
Public Use Permitted.
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