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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
19960020551
Acquisition Source
Headquarters
Document Type
Conference Proceedings
Authors
Foxlin, Eric
(Massachusetts Inst. of Tech. Cambridge, MA United States)
Date Acquired
September 6, 2013
Publication Date
April 3, 1996
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-CR 200870
NAS 1.26:200870
Report Number: NASA-CR 200870
Report Number: NAS 1.26:200870
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
Sponsors: Institute of Electrical and Electronics Engineers, Institute of Electrical and Electronics Engineers
Accession Number
96N24100
Funding Number(s)
CONTRACT_GRANT: NAGw-1322
Distribution Limits
Public
Copyright
Public Use Permitted.
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