NDLI: Gps/ins sensor fusion using gps wind up model

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Gps/ins sensor fusion using gps wind up model

Content Provider	NASA Technical Reports Server (NTRS)
Copyright Year	2013
Description	A method of stabilizing an inertial navigation system (INS), includes the steps of: receiving data from an inertial navigation system; and receiving a finite number of carrier phase observables using at least one GPS receiver from a plurality of GPS satellites; calculating a phase wind up correction; correcting at least one of the finite number of carrier phase observables using the phase wind up correction; and calculating a corrected IMU attitude or velocity or position using the corrected at least one of the finite number of carrier phase observables; and performing a step selected from the steps consisting of recording, reporting, or providing the corrected IMU attitude or velocity or position to another process that uses the corrected IMU attitude or velocity or position. A GPS stabilized inertial navigation system apparatus is also described.
File Size	1420948
Page Count	17
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_20150003147
Archival Resource Key	ark:/13960/t4hn07d9q
Language	English
Publisher Date	2013-11-05
Access Restriction	Open
Subject Keyword	Spacecraft Design, Testing And Performance Integers Attitude Inclination Patents Navigation Satellites Stabilization Inertial Navigation Global Positioning System Correction Position Errors Ambiguity Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Patent

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