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Course Information

Course Name
Turkish İleri Uçuş Dinamiği
English Advanced Flight Dynamics
Course Code
UUM 523E Credit Lecture
(hour/week)
Recitation
(hour/week)
Laboratory
(hour/week)
Semester -
3 3 - -
Course Language English
Course Coordinator Şükrü Akif Ertürk
Course Objectives 1. To develop conceptual understanding and technical insight into flight dynamics principles,
2. To introduce the methods to obtain the linear dynamics of the aircraft and to analyze the aircraft dynamics in terms of stability characteristics and flying and handling qualities,
3. To build up the necessary techniques for modeling the 6-DOF nonlinear aircraft dynamics and the simulation of the aircraft motion.
Course Description Coordinate systems and axes transformations, the aircraft equations of motion, the 6-DOF aircraft dynamics modeling and simulation, the aircraft static stability, the aircraft trim problem, linearization of the aircraft equations of motion, the aircraft longitudinal dynamics, the aircraft lateral-directional dynamics, the aircraft flying and handling qualities.
Course Outcomes By the end of the class students should be able to:

1. Comprehend the coordinate systems and axes transformations defined for aircraft dynamics,
2. Comprehend and derive the aircraft equations of motion including external forces and moments,
3. Comprehend and model the 6-DOF aircraft dynamics including the nonlinear effects and perform the simulation of the aircraft motion using the computer-based programming,
4. Have some knowledge of the basics of aircraft static stability,
5. Comprehend and perform the aircraft trim analyses,
6. Comprehend the methodology of the linearization and derive the linearized equations from nonlinear aircraft dynamics,
7. Derive the longitudinal equations and analyze the aircraft longitudinal motion,
8. Derive the lateral-directional equations and analyze the aircraft lateral-directional motion,
9. Have some knowledge about aircraft flying and handling qualities, standards and specifications.
Pre-requisite(s)
Required Facilities
Other
Textbook • Yechout, T. R., Introduction to Aircraft Flight Mechanics. AIAA, 2003.
Other References • Cook, M. V., Flight dynamics principles: a linear systems approach to aircraft stability and control. Butterworth-Heinemann, 2012.
• Napolitano, M. R., Aircraft Dynamics: From Modeling to Simulation. John Wiley & Sons, 2012.
• Nguyen, L. T., et al. Simulator Study of Stall/Post Stall Characteristics of a Fighter Airplane with Relaxed Longitudinal Static Stability. NASA Technical Paper 1538. Washington, D.C.: NASA, December 1979.
• De Marco, A., Eugene D., and Berndt, J., A general solution to the aircraft trim problem. In AIAA Modeling and Simulation Technologies Conference and Exhibit, p. 6703. 2007.
 
 
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