aileron angle

aileron angle

aileron angleclick for a larger image
The angle of deflection of an aileron from its neutral position. This angle is negative when the aileron's trailing edge is below its neutral position and positive when the trailing edge is above the neutral position.
An Illustrated Dictionary of Aviation Copyright © 2005 by The McGraw-Hill Companies, Inc. All rights reserved
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[mathematical expression not reproducible] is the control moment coefficient matrix subjected to the control surface, and u = [[[delta].sub.R], [[[delta].sub.A]].sup.T] is the control input, where [[delta].sup.R ]and [[delta].sup.A ]represent the rudder angle and aileron angle of the hydrofoil system, respectively.
The rudder angle and aileron angle of the two cases are presented in Figures 5 and 6.