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Flight Dynamics Principles, 2nd Edition
book

Flight Dynamics Principles, 2nd Edition

by Michael V. Cook
February 2011
Beginner to intermediate content levelBeginner to intermediate
488 pages
17h 21m
English
Butterworth-Heinemann
Content preview from Flight Dynamics Principles, 2nd Edition
Ch14-H6927.tex 20/6/2007 16: 39 Page 401
Coursework Studies 401
DESIGNING THE AILERON–RUDDER INTERLINK GAIN
(xv) The objective here is to design a suitable value for the interlink gain K
ari
for each
of the three flight conditions. This may only be done by choosing a test value and
including it in the input mixing matrix L in the closed loop model developed in
(xi), obtaining the transfer functions and observing the response to an aileron
command. The correct value of K
ari
is the minimum value that will cancel the
adverse sideslip response seen in the transient immediately following application
of the aileron command. Suitable values of gain lie in the range ...
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Publisher Resources

ISBN: 9780750669276