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.
Detailed course contents will be included in the course handout.
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.