Aircraft Systems Modeling
Model Based Systems Engineering in
Avionics Design and Aircraft Simulation
Henric Andersson
Linköping Studies in Science and Technology Licentiate Thesis No. 1394
Division of Machine Design
Department of Management and Engineering Linköpings universitet Out 1 1 Lookup Table Integer Delay -25 Z Discrete-Time Integrator K Ts z-1 In 1 1 Gear = 2 Inertia 1 J=1 Inertia 2 J=1.5 Torque 1 tau Torque 2 tau DriveSine freqHz ={1} Load duration={2}
LIU-TEK-LIC-2009:2 ISBN 978-91-7393-692-7 ISSN 0280-7971
Identification - Physical Object No:
Copyright © March 2009 by Henric Andersson Division of Machine Design
Department of Management and Engineering
Linköpings universitet, SE-581 83 Linköping, Sweden