DocumentCode :
804041
Title :
Analog sensitivity design of Saturn V launch vehicle
Author :
Rillings, James H. ; Roy, Rob J.
Author_Institution :
General Motors Research Laboratories, Warren, MI, USA
Volume :
15
Issue :
4
fYear :
1970
fDate :
8/1/1970 12:00:00 AM
Firstpage :
437
Lastpage :
442
Abstract :
This paper describes a useful method for limiting the sensitivity of high-order systems to unknown changes in specific parameters. A brief review of the development of sensitivity coefficients and the governing sensitivity equation is given. The desensitization problem is then formulated as an optimal control problem with a specified feedback structure and performance indices defined for both the state and sensitivity vectors. A method of iteratively finding the optimal feedback gains by simultaneous solution of the state and sensitivity equations via analog computer is described and an algorithm is given. This method of analog sensitivity design is then applied to a seventh-order model of a Saturn V booster with the frequency of the first bending mode serving as the unknown parameter. Analog sensitivity design is shown to produce a control system with sensitivity to the varying parameter greatly reduced over that of the corresponding system designed without using sensitivity considerations.
Keywords :
Sensitivity design; Space-vehicle launching; Analog computers; Control systems; Differential equations; Frequency; Iterative algorithms; Optimal control; Saturn; State feedback; Testing; Vehicle dynamics;
fLanguage :
English
Journal_Title :
Automatic Control, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9286
Type :
jour
DOI :
10.1109/TAC.1970.1099530
Filename :
1099530
Link To Document :
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