DocumentCode :
1410132
Title :
Appendixes to "Continuous Time-Varying Optimal Feedback Applied to the Augmentation and Rapid Alignment of Inertial Systems\´\´
Author :
Fagin, S.L. ; Grinoch, E. ; Graefe, A.
Author_Institution :
Sperry Gyroscope Company, Division of Sperry Rand Corporation, Great Neck, N. Y.
Issue :
3
fYear :
1967
fDate :
5/1/1967 12:00:00 AM
Firstpage :
555
Lastpage :
560
Abstract :
The original paper was presented at the IEEE/G-AES Aerospace Systems Conference, Seattle, Wash., July 11-15, 1966, and was published (less Appendixes) in the Supplement to this Transactions, vol. 2, no. 4, PP. 661-678, July 1966. The four appendices cover: The White Noise Case; A Common Start-Up Problem; Revised Vector Error-Propagation Block Diagram; and Two-Dimensional Model of Inertial System for the "Complete" Position (Or Velocity) Inertial and on Ground Alignment Problems.
Keywords :
Aerospace electronics; Covariance matrix; Equations; Feedback; Frequency; Gyroscopes; Navigation; Noise reduction; Time varying systems; White noise;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/TAES.1967.5408818
Filename :
5408818
Link To Document :
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