Unformatted text preview: from the following level-flight condition: altitude = 35,000 ft, airspeed = 850 ft/s, angle-of-attack = 1.88 deg, elevator = -1.78 deg, and thrust = 1600 lb. Problem 3 (10 pts) Find a linear model for the AUV. The control variables (u vector) include buoyancy, thrust, and all four tail fin deflections. Assume a level-flight equilibrium condition with speed = 1.5 m/s, depth = 50 m, buoyancy = 184.5 N, angle-of-attack = -1.06 deg, thrust = 8.2 N, fin_left = 4.3 deg, fin_right = 0.8 deg....
View Full Document
This note was uploaded on 01/18/2012 for the course MAE 142 taught by Professor Aliseda,a during the Spring '08 term at UCSD.
- Spring '08