DocumentCode :
1179197
Title :
A Settling Time Constrained Optimization of a Velocity Inertial Navigation System
Author :
Porter, W.A. ; Kuo, M.C.Y.
Author_Institution :
The Control Systems Research Unit of the Institute of Science and Technology, The University of Michigan, Ann Arbor, Mich.
Issue :
2
fYear :
1964
fDate :
6/1/1964 12:00:00 AM
Firstpage :
112
Lastpage :
117
Abstract :
In this paper, a description of a technique for improving transient performance in the velocity inertial system while minimizing the standard deviation of the system error, (i.e., standard deviation of the system velocity measurement error ¿v2) is given. To accomplish this objective, a prescribed settling time constraint is formulated for the system response. The constraint equation is then imposed on the minimization process. The result shows that considerable settling time improvement can be derived without sacrificing system accuracy.
Keywords :
Acceleration; Accelerometers; Constraint optimization; Equations; Helium; Inertial navigation; Measurement standards; Sensor phenomena and characterization; Time factors; Velocity measurement;
fLanguage :
English
Journal_Title :
Aerospace and Navigational Electronics, IEEE Transactions on
Publisher :
ieee
ISSN :
0096-1957
Type :
jour
DOI :
10.1109/TANE.1964.4502172
Filename :
4502172
Link To Document :
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