Lehrinhalte
Aircraft Stability and Dynamics
- static longitudinal motion (lift, pitching moment, neutral point,
manoeuvre point)
- static lateral motion (yaw moments, roll moments, state of flight:
steady sideslip manoeuvre, flight with only one engine, steady turn)
- dynamic longitudinal stability (stability axis system, linearized
equations of motion, Eigenvalues: short period mode, phugoid mode)
- dynamic lateral stability (linearized equations of motion,
Eigenvalues: rolling subsidence mode, spiral convergence/divergence
mode, dutch roll)

Literatur
U. Klingauf: Lecture Script
B. Etkin / L.D. Reid: Dynamics of Flight                     
R. Brockhaus / W. Alles / R. Luckner:  Flugregelung
T. R. Yechout:  Introduction to Aircraft Flight Mechanics
B.L. Stevens / F. F. Levis:  Aircraft Control and Simulation
J. D. Anderson:  Introduction to Flight
M. V. Cook: Flight Dynamic Principles

Voraussetzungen
Background in engineering mathematics (calculus, lineare algebra und differential equations), technical mechanics (statics and dynamics), fluid mechanics (incompressible flow) and systems theory (multivariable systems and state space) necessary.

Erwartete Teilnehmerzahl
75

Online-Angebote
moodle

Semester: ST 2018