Linear Parameter Varying Switching Attitude Tracking Control for a Near Space Hypersonic Vehicle Via Multiple Lyapunov Functions

Publisher: John Wiley & Sons Inc

E-ISSN: 1934-6093|17|2|523-534

ISSN: 1561-8625

Source: ASIAN JOURNAL OF CONTROL, Vol.17, Iss.2, 2015-03, pp. : 523-534

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Abstract