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Institution:
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Embry-Riddle Aeronautical University-Daytona Beach
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Subject:
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Description:
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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.
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Credits:
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3.00
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Credit Hours:
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Prerequisites:
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Corequisites:
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Exclusions:
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Level:
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Instructional Type:
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Lecture
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Notes:
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Additional Information:
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Historical Version(s):
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Institution Website:
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Phone Number:
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(800) 222-3728
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Regional Accreditation:
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Southern Association of Colleges and Schools
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Calendar System:
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Semester
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