NDLI: Integrated inertial/gps

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Integrated inertial/gps

Content Provider	NASA Technical Reports Server (NTRS)
Author	Kline, Paul Vangraas, Frank
Copyright Year	1990
Description	The presence of failures in navigation sensors can cause the determination of an erroneous aircraft state estimate, which includes position, attitude, and their derivatives. Aircraft flight control systems rely on sensor inputs to determine the aircraft state. In the case of integrated Inertial/NAVSTAR Global Positioning System (GPS), sensor failures could occur in the on-board inertial sensors or in the GPS measurements. The synergistic use of both GPS and the Inertial Navigation System (INS) allows for highly reliable fault detection and isolation of sensor failures. Integrated Inertial/GPS is a promising technology for the High Speed Civil Transport (HSCT) and the return and landing of a manned space vehicle.
File Size	264985
Page Count	6
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19910009719
Archival Resource Key	ark:/13960/t4gn33s5w
Language	English
Publisher Date	1990-12-01
Access Restriction	Open
Subject Keyword	Aircraft Communications And Navigation Civil Aviation Transport Aircraft Global Positioning System Derivation Flight Control System Failures Errors Attitude Inclination Faults Fault Detection Inertial Navigation High Speed Detection Failure Navigation Instruments Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Article

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