Search NASAโŒ• Search

NASA NTRS ยท 19960028781

Inertial head-tracker sensor fusion by a complementary separate-bias Kalman filter

Abstract

Current 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.

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Foxlin, Eric. 1996-01-01. Inertial head-tracker sensor fusion by a complementary separate-bias Kalman filter. https://ntrs.nasa.gov/citations/19960028781

Cite the original work for its findings. Save a collection to share your selection of sources.