Journal
JOURNAL OF SYSTEMS ENGINEERING AND ELECTRONICS
Volume 24, Issue 2, Pages 288-295Publisher
SYSTEMS ENGINEERING & ELECTRONICS, EDITORIAL DEPT
DOI: 10.1109/JSEE.2013.00036
Keywords
flexible air-breathing hypersonic vehicle; nonlinear robust controller; high order sliding mode control; output tracking control
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Funding
- National Natural Science Foundation of China [91016018, 61273092, 61203012]
- Foundation for Key Program of Ministry of Education of China [311012]
- Key Program for Basic Research of Tianjin [11JCZDJC25100]
- Key Program of Tianjin Natural Science [12JCZDJC30300]
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The focus of this paper is on control design and simulation for the longitudinal model of a flexible air-breathing hypersonic vehicle (FAHV). The model of interest includes flexibility effects and intricate couplings between the engine dynamics and flight dynamics. To overcome the analytical intractability of this model, a nominal control-oriented model is constructed for the purpose of feedback control design in the first place. Secondly, the multi-input multi-output (MIMO) quasi-continuous high-order sliding mode (HOSM) controller is proposed to track step changes in velocity and altitude, which is based on full state feedback. The simulation results are presented to verify the effectiveness of the proposed control strategy.
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