Course Information

Course Name	Turkish	Advanced Flight Dynamics
	English	Advanced Flight Dynamics
Course Code	UUM 523E	Credit	Lecture (hour/week)	Recitation (hour/week)	Laboratory (hour/week)
Semester	-	3	-	-	-
Course Language		English
Course Coordinator		Hayri Acar
Course Objectives		1- Numerical Calculations on Aircraft Dynamics will be performed for better understanding of the topic. 2- Various programming technics which can be used for flight dynamics analyses will be explained 3- Various available or in class developed computer programs written in FORTRAN or other languages will be used for flight simulations and investigating the aircraft dynamic stability, control and flight performance.
Course Description		Aircraft Equations of Motion; Aerodynamic and Thrust Forces and Moments; Aircraft three and six degree of freedom trim analyses; Time dependent Numerical Solution of the Nonlinear Aircraft Equations of Motion; Simulation of Various Flight Scenarios; Linearization of the Equations of Motion; Aircraft Dynamic Stability
Course Outcomes		M.Sc./Ph.D. students who successfully pass this course gain knowledge, skill and competency in the following subjects; 1-To obtain aircraft equations of motion 2-To program and use an atmosphere model 3-To model aerodynamic, thrust and mass forces and moments 4-To perform three or six degree of freedom aircraft trim analyses 5-To perform flight simulations based on numerical solution of nonlinear aircraft equations of motion 6-To be able to derive linearized aircraft equations and be acquainted with them 7-To have knowledge on dynamic stability characteristics of aircraft
Pre-requisite(s)
Required Facilities
Other
Textbook		Yechout T.R., Morris S. L., Bosserties D. E., Hallgren W. F., “Introduction to Aircraft Flight Mechanics: Performance, Static Stability, Dynamic Stability and Classical Feedback Control”, AIAA Education Series, 2003
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