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Recent advances in strapdown inertial navigationThe computational requirements and basic features of strapdown gyroscopes for inertial navigation are discussed. Strapdown navigators currently require 20 to 50% of the available time of a minicomputer with a capability of several hundred thousand operations per second; memory requirements are 2000 to 3000 16-bit words. A system in which these computational demands are met by three limited capability microcomputers is described. A technique using dedicated microprocessors in the place of analog electronics in the gyroscope control loops is discussed, and attention is given to applications of microprocessor technology in redundant strapdown navigation systems and associated flight control systems.
Document ID
19760028874
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Napjus, G. A.
(Teledyne Systems Co. Northridge, Calif., United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Subject Category
Aircraft Communications And Navigation
Meeting Information
Meeting: INTERCON 75
Location: New York, NY
Start Date: April 8, 1975
End Date: April 10, 1975
Accession Number
76A11840
Funding Number(s)
CONTRACT_GRANT: NAS1-12175
CONTRACT_GRANT: NAS1-13088
Distribution Limits
Public
Copyright
Other

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