Attitude control for reentry reusable launch vehicle

This paper investigates the robust feedback control problem associated with finite time attitude stabilization of a reentry reusable launch vehicle subject to plant uncertainties and external disturbance. An integral terminal sliding mode is proposed firstly to achieve finite time stability in the s...

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Bibliographic Details
Published inChinese Control and Decision Conference pp. 5633 - 5636
Main Authors Jianguo, Guo, Guoqing, Wang, Jun, Zhou
Format Conference Proceeding Journal Article
LanguageEnglish
Published IEEE 01.05.2016
Subjects
Aerodynamics
Attitude control
Composite Control
Control systems
Electronics
Finite-time Convergence
Integrals
Mathematical analysis
Mathematical model
Reentry
Reentry Vehicle
Reusable launch vehicles
Robustness
Sliding Mode
Terminals
Vehicle dynamics
Vehicles
Online AccessGet full text
ISSN1948-9447
DOI10.1109/CCDC.2016.7532005

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Summary:This paper investigates the robust feedback control problem associated with finite time attitude stabilization of a reentry reusable launch vehicle subject to plant uncertainties and external disturbance. An integral terminal sliding mode is proposed firstly to achieve finite time stability in the sliding mode. Then, a robust attitude control for a reentry reusable launch vehicle is derived using the designed integral terminal sliding mode, and the attitude of the reentry reusable launch vehicle can converge to the equilibrium in a finite time with composite actuators. Numerical simulations illustrate the reentry reusable launch vehicle performance obtained under the proposed controller.
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SourceType-Conference Papers & Proceedings-2
ISSN:1948-9447
DOI:10.1109/CCDC.2016.7532005