TU Berlin

Flight Mechanics, Flight Control and AeroelasticityFlight Mechanics II (Flight Dynamics)

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Flight Mechanics II (Flight Dynamics)

Content

Lupe

After assuming the aircraft as a point mass in Flight Mechanics it is described as a rigid, three dimensional body in Flight Mechanics 2. For this purpose further coordinate systems are introduced and the forces and moments in the longitudinal and lateral motion are discussed. Then the linearization of the nonlinear differential equations of motion around a steady state, which was determined by a trim calculation, is carried out. The linear systems of equations are analysed and the dynamic of the aircraft in longitudinal and lateral motion is explained.

Organization

Semester
Summer Semester
Language
English
Day / Time
Wednesday + Thursday, 12:15 -13:45
Room
F 11
ECTS
6
Lecturer
Prof. Dr.-Ing. Flávio Silvestre
Trainer
Caroline Schlemmer, M.Sc.
Type of examination
Portfolio (weekly Homework assignments + written exam)
Admission criterion
-
Module description
MTS

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