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Material Type: Assignment; Class: Flight Dynamics And Control; Subject: AAE-Aero & Astro Engineering; University: Purdue University - Main Campus; Term: Spring 2011;
Typology: Assignments
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April 12, 2011
Due: Monday, April 18
Exercise 1 This exercise refers to the figure with aircraft and propeller.
(a) Find eRb. Also, obtain eω¯b^ by inspection.
(b) Find bRc. Also, obtain bω¯c^ by inspection.
(c) Compute eRc.
(d) Compute eΩc
(e) Using eΩc^ from part (d), compute e^ ω¯c^ and compare this to e^ ¯ωb^ + b^ ω¯c^ as computed from parts (a) and (b).
Exercise 2 The linearized lateral dynamics of an F-16 about a trim condition corresponding to straight and level flight at 502 ft/s can be described by δ x˙ = Aδx where x = (β, φ, p, r) and
(From Steven and Lewis, 2nd ed, p. 210) Identify the eigenvalues and eigenvectors corresponding to the dutch roll mode, the roll subsidence mode and the spiral mode.
