Journal
SCIENCE CHINA-INFORMATION SCIENCES
Volume 54, Issue 3, Pages 563-576Publisher
SCIENCE PRESS
DOI: 10.1007/s11432-011-4201-3
Keywords
FSPM; multi-objective robust control; intelligent control; hypersonic vehicle
Funding
- National Science Fund for Distinguished Young Scholars [60625304]
- National Natural Science Foundation of China [90716021, 60621062]
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In this paper, we propose a multi-objective robust controller based on fuzzy singularly perturbed models (FSPM) for the longitudinal motion of an air-breathing hypersonic vehicle. The control objective is to provide velocity and altitude tracking in the presence of the uncertainties and unknown nonlinearities in the model caused by variations in flight conditions. By approximating the multi-time-scale model with FSPM, ill-posed matrix calculations are circumvented. Under this framework, a fuzzy multi-objective robust controller is developed, and the linear matrix inequalities (LMI) condition is derived. Numerical simulation using the longitudinal model of a hypersonic aircraft is provided to demonstrate the effectiveness of the proposed strategy.
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