MAE 5070

Dynamics of Flight Vehicles

Course Description

Course information provided by the 2018-2019 Catalog.

Introduction to stability and control of atmospheric-flight vehicles. The dynamics governing the motion of aircrafts are explored through a series of case studies, each focusing on different flight stages or configurations. Review of aerodynamic forces and methods for analysis of linear systems. Static stability and control. Small disturbance equations of unsteady motion. Dynamic stability of longitudinal and lateral-directional motions; transient response. Simulation of large motions of aircrafts.

Prerequisites/Corequisites Prerequisite: MAE 3050, MAE 3230, and MAE 3260 concurrently or permission of instructor.

Outcomes

• Students will understand the nature of aerodynamic forces and moments (aerodynamic stability derivatives) in determining the motions of a flight vehicle.
• Understand the various terms in the equations of motion and the simplifications arising from assumptions of small disturbances from equilibrium flight and from the bi-lateral symmetry of most aircraft.
• Be able to identify, formulate and solve engineering problems in aircraft flight dynamics.
• Understand the principal constraints imposed on aircraft design by stability and controllability requirements.

When Offered Spring.

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