For fixed-wing aircraft longitudinal motions, it is often desirable to use the stability-frame instead of the body-fixed
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For fixed-wing aircraft longitudinal motions, it is often desirable to use the stability-frame instead of the body-fixed frame, as shown in the figure, where Vr = √²+w² is the true air speed, which is the magnitude of the body-frame velocity under no wind condition, and a = tan-¹. Note that u Vtcosa, w = Vtsina.
r
Use the body-frame longitudinal translational EOM
to derive the stability-frame translational EOM
Related Book For
Introductory Statistics For The Behavioral Sciences
ISBN: 9780470907764
7th Edition
Authors: Joan Welkowitz, Barry H. Cohen, R. Brooke Lea
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