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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 101
The Solution of the Equations of Motion 101
and
x
3
=
12y
1
24y
2
35y
3
123
245
356
=
y
1
24
35
y
2
12
35
+y
3
12
24
1
= 2y
1
y
2
Clearly, in this example, the numerator determinants are found by expanding about
the column containing y. The denominator determinant may be found by expanding
about the first row thus
123
245
356
= 1
45
56
2
25
36
+3
24
35
=−1 +6 6 =−1
5.3 AIRCRAFT RESPONSE TRANSFER FUNCTIONS
Aircraft response transfer functions describe the dynamic relationships between the
input and output variables.The relationships are indicated diagrammaticallyin ...
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Publisher Resources

ISBN: 9780750669276