LMS Amesim for the aerospace industry - A selection of theses and papers

Realize innovation.Unrestricted © Siemens AG 2017
LMS Imagine.Lab Amesim
for the aerospace industry
A selection of theses and papers LMS Imagine.Lab Amesim™
A world leading platform for physical
simulation of mechatronic systems

Unrestricted © Siemens AG 2017
Page 2 Siemens PLM Software
Scalable multiphysics behavioral modeling and analysis
LMS Amesim
45 libraries
5,000 multi-physics models
Fluids EnergyThermodynamics Control Liquid
propulsion
Mechanical Electrical
High-fidelity plant models (SIL, HIL)
Support of real-time platfroms
Standards
Interfaces to simulation
Multiple 3D CAE
Applications
Open, mechatronics simulation platform
Scalable
system
to
component
Flight controls Flight
dynamics
Environmental
control system
Fuel systems Electrical
systems
Landing gear Propulsion
systems
Engine
equipment
Integrated
systems
Hydraulic
systems

Cloud
Licensing
flexibility
Simcenter™ Portfolio for Predictive Engineering Analytics
Cornerstones for a future-proof engineering approach
Covering full range of
methods
Analytics, reporting &
exploration
Deployment flexibility
Openness &
Scalability
User experience
Industry &
engineering expertise
Systems approach
Collaboration &
workflow
Multidiscipline
& multiphysics
R
F
L
P
Controls
1D
3D
TEST
CFD

Agenda
•LMS Amesim for all types of
aircraft
• Airplane
• Unmanned Aerial Vehicle (UAV)
• Helicopter
• Spacecraft
•LMS Amesim for all
functions and subsystems
•Going further

L. Wang – INSA Toulouse – France – [ thesis ]
Force fighting for active/active redundant actuation system

M. Hutchison – Airbus Operations SAS – France – [ paper ]
Jet engine fuel system integration in aircraft environment

“Results show that the experiment matches well with the
simulation with a relative error no more than 5% and that
0–50 °C fuel temperature variation produces up to 5.2%
decrease in fuel rate”
B. Wang – Nanjing University of Aeronautics and Astronautics –
[ paper ]
Study of temperature effect on servovalve-controlled fuel metering unit

Agenda
aircraft
• Airplane
• Helicopter
• Spacecraft
•Going further

D. Cazangiu and al. - Transilvania University of Brasov – Romania
– [ paper ]
Investigation of the UAV electrical network

Vives – KULAB – LMS International – Belgium – [ paper ]
Real-time simulation of an integrated electrical system of a UAV

T. Andrieu, G. Frichet – LMS International – France – [ paper ]
Design and test quadcopters

Agenda
aircraft
• Airplane
• Helicopter
• Spacecraft
•Going further

T. Marger – ENSAM ParisTech – France – [ thesis ]
Valve design of hydro-mechanical servoactuator

P. Silvestri – Genova University – Italy – [ paper ]
Dynamic analysis of an helicopter rotor and control through co-
simulation

Agenda
aircraft
• Airplane
• Helicopter
• Spacecraft
•Going further

S. Ricci – Bologna University – Italy – [ paper ]
Virtual shaker testing for improving vibration test performance

A. Chaix and All – Thales Alenia Space – France – [ paper ]
Thermal dissipation management of spacecraft

Agenda
aircraft
• Flight controls
• Environmental control systems
• Fuel systems
• Electrical systems
• Landing systems
• Hydraulic systems
• Propulsion systems
•Going further

T. Rave and al. – Hamburg-Harburg TU – Germany – [ paper ]
Integrated thermal-dynamic analysis of airplane hydraulic systems

G. Altare – A. Vacca – Purdue University – USA – [ paper ]
Efficient and compact electro-hydraulic actuators

F. Jian – F. Yongling – Beihang University – China – [ paper ]
Flight control electromechanical actuators

W.L. Qin and al. - Beihang University – China – [ paper ]
Aileron actuator fault diagnosis