MAE 4183 Aircraft Stability & Control
The linearized equations of motion for atmospheric flight are developed. Longitudinal and lateral motions of the airplane are studied with particular emphasis on the phugoid, short-period, dutch-roll, and spiral motions. Static stability and control requirements for airplane design are considered. Prerequisite:
MA 233,
MAE 473,
MAE 4023
Lab Hours
0
Lecture Hours
3