- Schedule of Classes - June 22, 2015 4:42PM EDT
- Course Catalog - June 11, 2015 6:21PM EDT
Course information provided by the Courses of Study 2014-2015.
Introduction to stability and control of atmospheric-flight vehicles. 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. At the level of Flight: Stability and Automatic Control by Nelson.
When Offered Spring.
Prerequisites/Corequisites Prerequisite: MAE 3050. Prerequisite or corequisite: MAE 3260 or permission of instructor.
- 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.
Regular Academic Session.
Credits and Grading Basis
3 Credits Graded(Graded)
Class Number & Section Details
- TR Phillips Hall 219
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