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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| Published in | Chinese Control and Decision Conference pp. 5633 - 5636 |
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| Main Authors | , , |
| Format | Conference Proceeding Journal Article |
| Language | English |
| Published |
IEEE
01.05.2016
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| Subjects | |
| Online Access | Get full text |
| ISSN | 1948-9447 |
| DOI | 10.1109/CCDC.2016.7532005 |
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| Abstract | 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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| AbstractList | 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. |
| Author | Guo Jianguo Wang Guoqing Zhou Jun |
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| SubjectTerms | 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 |
| Title | Attitude control for reentry reusable launch vehicle |
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