2. Determine the transfer function from aileron deflection to roll rate in a F-104A aircraft. Assume the airplane is flying at sea level at a speed of 87m/sec. The F104A has the following aerodynamic and geometric data: Mass moment of inertia about the roll axis: I, = 4676kg m² Roll damping: 6079N m/rad/sec Roll moment from aileron control input: 380N m/deg
2. Determine the transfer function from aileron deflection to roll rate in a F-104A aircraft. Assume the airplane is flying at sea level at a speed of 87m/sec. The F104A has the following aerodynamic and geometric data: Mass moment of inertia about the roll axis: I, = 4676kg m² Roll damping: 6079N m/rad/sec Roll moment from aileron control input: 380N m/deg
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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Transcribed Image Text:2. Determine the transfer function from aileron deflection to roll rate in a F-104A
aircraft. Assume the airplane is flying at sea level at a speed of 87m/sec. The F104A
has the following aerodynamic and geometric data:
Mass moment of inertia about the roll axis: I, = 4676kg m?
Roll damping: 6079N m/rad/sec
Roll moment from aileron control input: 380N m/deg
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