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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 772A Linear Quadratic Integral Design Approach for...

A Linear Quadratic Integral Design Approach for the Automatic Control System of a Launch Vehicle

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Abstract:

This paper presents a design approach for the automatic flight control system of a launch vehicle using a linear quadratic integral technique together with a fixed gain Kalman filter. Its purpose is to analyse the stability and tracking robustness performances of the control system designed via this approach when atmospheric disturbances, modeling uncertainties and structural flexible modes of the launcher are taken into account.

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Periodical:

Applied Mechanics and Materials (Volume 772)

Pages:

410-417

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.772.410

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Online since:

July 2015

Authors:

Adrian Mihail Stoica*, Cristian Emil Constantinescu, Silvia Nechita

Keywords:

Automatic Flight Control, Kalman Filtering, Launch Vehicle, Optimal Linear Quadratic Integral Control Law

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© 2015 Trans Tech Publications Ltd. All Rights Reserved

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* - Corresponding Author

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