Adaptive Backstepping Flight Control for Modern Fighter Aircraft
InTech eBooks2011
Citations Over TimeTop 1% of 2011 papers
Abstract
F by a rotation of β -; and the body-fixed reference frame B F , obtained from S F by a rotation of α , as is also indicated in Fig. 1.The body-fixed reference frame B F can also be obtained directly from O F by three successive rotations of yaw
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