飞机改出尾旋控制规律研究

Abstract

Abstract: Based on the Bifurcation Analysis and Catastrophe Theory Methodology(BACTM), and by using the full six-degree-of-freedom nonlinear equations of motion, the characteristics of the equilibrium surfaces were analysed and the control techniques for aircraft spin recovery were studied in this paper. Some physical explanations were also given. With the employment of the Pontryagin Maximum Principle, the optimal treatment was carried out on the control history of spin recovery developed by BACTM, and the most rapid spin recovery control history was obtained. Based on this result, a suboptimal spin recovery technique has been founded.

Key words: spin, Bifurcation Analysis and Catastrophe Theory, optimiza-lion

Liu Chang;Jiang Ming. A STUDY OF THE CONTROL TECHNIQUE FOR AIRCRAFT SPIN RECOVERY[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1990, 11(2): 1-9.

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A STUDY OF THE CONTROL TECHNIQUE FOR AIRCRAFT SPIN RECOVERY

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