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A robust adaptive nonlinear control approach to missile autopilot design

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Keywords: Adaptive control; Missile autopilot; Nonlinear control

Document Type: Research Article

DOI: http://dx.doi.org/10.1016/S0967-0661(03)00016-9

Affiliations: Agency for Defense Development, 3-1-3, P.O. Box 35-3, Yuseong, , 305-600, Daejon, South Korea

Publication date: February 1, 2004

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