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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
Ch05-H6927.tex 20/6/2007 16: 34 Page 112
112 Flight Dynamics Principles
and applying the initial value theorem to obtain
θ(t)
t0
= Lim
s→∞
4.664(s +0.135)(s +0.267)
(s
2
+0.033s +0.022)(s
2
+0.893s +4.884)
deg = 0
(5.37)
Clearly, the values given by equations (5.36) and (5.37) correlate reasonably well with
the known pitch attitude response calculated in Example 5.3. Bear in mind that in all
the calculations numbers have been rounded to three decimal places for convenience.
5.5 ACCELERATION RESPONSE TRANSFER FUNCTIONS
Acceleration response transfer functions are frequently required but are not given
directly by the solution of the equations of motion described ...
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Publisher Resources

ISBN: 9780750669276