Skip to main content

AE322A: Aircraft Control Systems

Course Description

This course is a continuation of the previous semester's course, i.e. AE321A (Flight Mechanics). It will cover topics from Static flight stability, Equations of Motion, Dynamic flight stability, Control theory and Aircraft Control Systems.

Course Content

Detailed course contents will be included in the course handout.

Course Audience

It is all undergraduate students, primarily from Aerospace Engineering department and a couple of them from Mechanical Engineering department.

Outcomes of this Course

To learn about Static and Dynamic Flight Stability, Aircraft Equations of Motion and Control Theory as applied to aircraft flight dynamics.