Flight Mechanics & Controls
Lecture
Main Campus
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.
AA 173
Units: 3
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Typically Offered
Not Available
Grading Basis
Letter (ABCD/NP)
Class Level
Undergraduate
Instructional Mode
In Person
Gen Ed Requirement(s)
None