Flight Mechanics & Controls
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Course Description
Aircraft flight dynamics, stability, and their control system design; frame transformations, non-linear equations of motion for aircraft; linearization of longitudinal and lateral-directional dynamics; aircraft static longitudinal and lateral/directional stability and control; observability and controllability; PID feedback control; Prerequisites: E15, E105, AA100 and familiarity with MATLAB.
Grading Basis
RLT - Letter (ABCD/NP)
Min
3
Max
3
Course Repeatable for Degree Credit?
No
Course Component
Lecture
Enrollment Optional?
No
Does this course satisfy the University Language Requirement?
No
Programs
AA173
is a
completion requirement
for: