摘要

This paper presents a new stabilizing control law for a planar vertical take-off and landing aircraft. The model is first transformed into an equivalent form, and then a control law consisting of a linear term and a saturated term is given for a related subsystem, with the saturation levels being assigned as large as possible. Compared to the existing saturation scheme in which all states are restricted by saturations, the design brings about a relatively fast convergence. The effectiveness and advantage of the design are validated by numerical simulations. ? 2011 South China University of Technology, Academy of Mathematics and Systems Science, Chinese Academy of Sciences and Springer-Verlag Berlin Heidelberg.

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