NDLI: GPS-INS data integration for remote sensing

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GPS-INS data integration for remote sensing

Content Provider	IEEE Xplore Digital Library
Author	Gibson, J.R. Schwarz, K.P. Wei, M. Cannon, M.E.
Copyright Year	1992
Description	Author affiliation: Canada Center for Remote Sensing, Oattawa, Ont., Canada (Gibson, J.R.)
Abstract	Summary form only given, as follows. Flight tests have been performed for the purpose of assessing the use of post-mission integrated data from GPS (Global Positioning System) and INS (inertial navigation system) systems for remote sensing applications. While GPS data alone are sufficient for aircraft guidance, they do not currently satisfy the requirement for position and attitude information at high data rates, with typical sampling times between 5 and 40 ms. This information is needed for image processing applications where data discontinuities greater than a few centimeters in the positions must be avoided. The authors describe the test design which provided for multiple GPS stations on the ground from which the GPS receiver in the aircraft was monitored. The airborne GPS receiver was precisely synchronized with the stable platform INS. The accuracy of position, velocity, and attitude was analyzed using different approaches to post-mission data integration. These results were then used to georeference the imagery from the Multiple-Detector Electro-Optical Imaging Scanner and to compare it to independent ground truth.
File Size	35913
File Format	PDF
ISBN	0780304683
DOI	10.1109/PLANS.1992.185889
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	1992-03-23
Publisher Place	USA
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Remote sensing Global Positioning System Data acquisition Aerospace engineering Data engineering System testing Performance evaluation Image sampling Image processing Aircraft
Content Type	Text
Resource Type	Article

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