MAE 457
Flight Vehicle Stability and Control
Section: 002

Course Description

Longitudinal, directional and lateral static stability and control of aerospace vehicles. Lineralized dynamic analysis of the motion of a six degree-of-freedom flight vehicle in response to control inputs and disturbance through use of the transfer function concept. Control of static and dynamic behavior by vehicle design (stability derivatives) and/or flight control systems.

Spring 2025

Instructors

Meeting Patterns

Classes Start:
January 6, 2025
Classes End:
April 22, 2025
Location:
02232 Engineering Building 3
Class Days:
M W
Class Start Time:
11:45am
Class End Time:
1:00pm

Class Type:
Lecture
Credits:
3.00
Restrictions:
P: (MAE 252 or MAE 308) AND (MAE 315 or MAE 361)