SIM 300 - Flight Dynamics Algorithms

Institution:
Embry-Riddle Aeronautical University-Daytona Beach
Subject:
Description:
3 Credits This course will derive the equations of motion of a 6 DOF aerospace vehicle. Stability derivative will be defined mathematically. The equations for static and dynamic stability of the longitudinal and lateral directional motion will be derived. Numerical integration methods in a suitable computer language will be used to solve these equations. Physical understanding of stability derivates will be discussed at length. Prerequisite: MA 345. Corequisite: AE 302.
Credits:
3.00
Credit Hours:
Prerequisites:
Corequisites:
Exclusions:
Level:
Instructional Type:
Lecture
Notes:
Additional Information:
Historical Version(s):
Institution Website:
Phone Number:
(800) 222-3728
Regional Accreditation:
Southern Association of Colleges and Schools
Calendar System:
Semester

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