stirling ima conference presentation - modelling and simulation
DESCRIPTION
An overview of typical modelling and simulation activities performed by Stirling Dynamics. Over the years, Stirling’s fluid systems modelling capability has typically embraced flight control systems, landing gear systems and fuel systems.TRANSCRIPT
Stirling Dynamics
Modelling and
Simulation
Int roduct ion
• Specialist engineering and design services
• Mechatronic systems
• Serving aerospace, marine, energy and defence
• 26+ years trading history
• US and UK bases
• Focus on innovation and value
© 2014 Stirling Dynamics
3
B u s i n e s s Fo c u s
© 2014 Stirling Dynamics
Training &
Simulation
Active Hand
Controls
G-Seats
Pallet Solutions
Standard
Products
Custom Designs
Aerospace
Services
Modelling and
Simulation
Landing Gear
Systems
Structures &
Materials
Flight Sciences
Test Services
Submarine
Systems
Steering & Diving
Control Systems
Submarine
Autopilots
Hover Systems
Systems
Engineering
Trials Support
Energy Systems
Condition
Monitoring
System
Water Purification
Systems
Sub Sea Analysis
Office Locations
© 2013 Stirling Dynamics 4
Orlando
Seattle
Farnborough
Bristol
Yeovil
O f f i c e L o c a t i o n s
© 2014 Stirling Dynamics
U S a n d U K b a s e s
Major Customers
M a j o r C u s t o m e r s
© 2014 Stirling Dynamics
© 2008 Stirling Dynamics 6
M o d e l l i n g a n d S i m u l a t i o n C a p a b i l i t y
D y n a m i c s , C o n t r o l a n d Pe r f o r m a n c e
© 2014 Stirling Dynamics
Core Stirling capability:
• 20+ engineers (10 PhDs)
• Mathematical modelling of mechanical, hydraulic, pneumatic and
electrical systems
• Analysis of kinematics, dynamics, stability and control
Capability applied to:
• Fuel systems
• Landing gear systems
• Flight control systems
Modelling and analysis frequently lends itself to off-site packaging:
• Fully delegated service – all skills and tools available in-house
• All processes adhere to AS/EN9100, ISO 9001
A e r o s p a c e S e r v i c e s – E n g i n e e r i n g
M o d e l l i n g a n d S i m u l a t i o n C a p a b i l i t y
D y n a m i c s , C o n t r o l a n d Pe r f o r m a n c e
Robust approach to modelling and simulation:
• Requirements capture and decomposition
• Model specification
• Verification and validation planning
System performance analysis:
• Steady state and transient behaviour
• Time domain and frequency domain analysis
• Normal operation and failure mode analysis
© 2014 Stirling Dynamics
© 2008 Stirling Dynamics 8
M o d e l l i n g a n d S i m u l a t i o n C a p a b i l i t y
D y n a m i c s , C o n t r o l a n d P e r f o r m a n c e
© 2014 Stirling Dynamics
Industry standard tools:
• Matlab, Simulink
• SimScape,
SimMechanics,
SimHydraulics
• Real-Time Workshop
(e.g. for xPC, VxWorks,
RTLinux targets)
• EASY5, AMESim
• ADAMS
• LabView
© 2014 Stirling Dynamics
Software development:
• HTML
• JavaScript
• SQL
• Fortran
• C, C++
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© 2014 Stirling Dynamics
M e c h a n i c a l S y s t e m s
I n - F l i g h t R e f u e l l i n g H o s e S i m u l a t i o n
In-Fight Refuelling Hose Simulation:
• Dynamic hose response in flap vortex wake
• Modelling of hose mechanical properties
• Modelling of aerodynamic lift and drag
• Model validation against wind tunnel data
• De-risk new aircraft design
2
Out
1
In
B F
Revolute Joint
1/s
[alpha]
CS1
CS4
CS2
CS3
CG
Element Mass
v
Body Sensor
(local axis)
av
Body Sensor
(World axis)
Body Actuator
Measurements Torque
Bending Stiffness and Damping
Body x v elocity
Body y v elocity
Angle rel to Earth
Ux
Uy
alpha
Airstream Velocity Calculations
Ux
Uy
Fy
Fx
Aero Loading
Body axis x v elocity
Body axis y v elocity
Angle relativ e
to Earth
Fy
Fx
Body axis loads
10
© 2014 Stirling Dynamics
H y d r a u l i c S y s t e m s
F i g h t C o n t r o l s , L a n d i n g G e a r a n d Fu e l
S y s t e m s
Modelling analysis support:
• Airframe manufacturers (system integrators)
• Systems suppliers (e.g. landing gear, flight controls)
Electronic Control
Unit
LVDT
Power Drive
Electronics
Duplex Valve
Duplex Actuator
Position
Demand
Aircraft Hydraulic Supply 1
Aircraft Hydraulic Supply 2
LVDT
Valve
Coil Power Drive
Electronics
Electronic Control
Unit
Applied Load
• Flight Control Systems
• Landing Gear Systems
• Fuel Systems
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© 2014 Stirling Dynamics
H y d r a u l i c S y s t e m s
P r i m a r y F l i g h t C o n t r o l s
Basic Analysis:
• Preliminary design review
• Linear modelling
• Simplex representations
• Design concept evaluation
ramVelocity
2
ramPosition
1PSS
Unequal spool
P
Pr
xv
A
B
Supply
Pressure
-C-
f(x)=0PSS
PSS
PSS
Mechanical
Load
R
C
E
Ideal Hydraulic
Pressure Source
S
TP
Double -Acting
Hyraulic Actuator
A
B
P
V
R
C
Custom Hydraulic
Fluid
valvePosition
1
0 0.05 0.1 0.15 0.2 0.25 0.3 0.35 0.4 0.450
0.2
0.4
0.6
0.8
1
1.2
1.4
Step Response
Time (sec)
Am
plit
ude
-80
-60
-40
-20
0
20
Magnitu
de (
dB
)
100
101
-720
-540
-360
-180
0
Phase (
deg)
Bode Diagram
Gm = 11.8 dB (at 6.4 Hz) , Pm = 66.6 deg (at 1.69 Hz)
Frequency (Hz)
Detailed Analysis:
• Critical design review
• Fluid friction, non-linear flow, temperature dependency
• Multiplex design
• Failure mode performance
• Non-linear frequency response
• Control system design
• Comprehensive performance evaluation against
requirements
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© 2014 Stirling Dynamics
H y d r a u l i c S y s t e m s
L a n d i n g G e a r S y s t e m – S i m u l i n k /
S i m H y d r a u l i c s
Dynamic representations of:
• Servo-valve
• By-pass valve
• Accumulator piston
• Hydro-mech model of steering system
• Required to establish baseline aircraft level
performance
• Steer, tow and free-to castor modes
0 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.8 2
-5
0
5
10
15
20
25
NLG
Time [s]
Th
eta
[d
eg
]
thetaTT
thetaST
Command
0 0.2 0.4 0.6 0.8 1 1.2 1.4 1.6 1.8 2
-10
0
10
20
30
40
Time [s]
W [d
eg
/s]
wTT
wST
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© 2014 Stirling Dynamics
H y d r a u l i c S y s t e m s
L a n d i n g G e a r E x t e n d S e q u e n c i n g A n a l y s i s –
E A S Y 5
Analysis accounting for:
• Temp range -50 to +90 C
• Laminar/turbulent flow
• Dissolved air and cavitation
• In-service problem
• Modification for improved sequencing of
ext/ret actuator and uplocks
• Modelling and analysis to support sizing of
new sequencing canisters
14
© 2014 Stirling Dynamics
C o - S i m u l a t i o n o f H y d r o - M e c h a n i c a l S y s t e m s
L a n d i n g G e a r E x t e n d a n d R e t r a c t – A D A M S a n d
A M E S i m
Co-simulation of mechanics and hydraulics
• ADAMS – flexible multi-body kinematics
• AMESim – detailed hydraulic performance
Modelling of full extend/retract system
• Landing gear, doors, ramps guides, hydraulics
• Flexible landing gear and doors
• Aerodynamics, joint frictions, contacts
Performance analysis of integrated system
• Performance under “normal” operation
• Failure mode performance (free-fall, missing tyre, missing wheel,
uplock failure, pitch trimmer failure and combinations)
• Loads analysis
• Support to certification
© 2014 Stirling Dynamics
A i r c r a f t Fu e l S y s t e m s
D i s p e n s e P u m p P r e s s u r e C o n t r o l Pe r f o r m a n c e
Requirement for closed loop pressure control:
• Development and validation of dispense pump
Requirements:
• Pump hydrodynamic model
• Controller functional and analogue
electronic design
• Validation of existing and revised pump
controller design
0 10 20 30 40 50 600
5
10
15
20
25
30
35
40
45
50
T/hr
Eta
(%
)
Hydraulic Efficiency Vs Flow
2200rpm
4400rpm
6600rpm
8800rpm
• Key interface between customer design team and
manufacturer
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A i r c r a f t Fu e l S y s t e m s -
A c c u m u l a t i o n a n d Tr a n s p o r t a t i o n o f Wa t e r i n
Fu e l
Development of an analysis tool for modelling the accumulation and transportation of water
within an aircraft fuel system:
mw ma
wallwm _
Pull, SHull,, Vull, Tull
downm *
* Positive flow directions
Pup, SHup
flowup SHm ,
SAE International
Wright Brothers medal winner
• Model accounting for; condensation, suspension,
dissolution and transportation
• Analysis tool for evaluating water management
requirements for different flight missions and the
impact of inerting systems on water management
© 2014 Stirling Dynamics
© 2014 Stirling Dynamics
M e c h a n i c a l a n d H y d r a u l i c S y s t e m s
S u m m a r y
Mechanical and hydraulic simulation
capability:
• Simulation models developed
alongside the design
• Comprehensive assessment of
system performance – normal
and failure modes
• Models fully documented and
tested
Mechanical and hydraulic simulation
support applied to:
• Airbus fuel system closed loop pressure control
• Airbus fuel systems R&T water management
modelling
• Airbus landing gear extend/retract and steering
systems
• FRL in-flight refuelling hose dynamics
• BAE Systems active pilot controls
• Bombardier landing gear systems
• Claverham primary flight control actuator (fixed
and rotary wing)
• APPH primary flight control actuator (rotary
wing)
Head Office UK
Stirling Dynamics Limited
26 Regent Street
Clifton
Bristol BS8 4HG
United Kingdom
Tel +44 (0)117 915 2500
Head Office US
Stirling Dynamics Inc.
4030 Lake Washington Blvd NE #205
Kirkland, WA 98033-7870
USA
Tel +1 (425) 827 7476
w w w . s t i r l i n g - d y n a m i c s . c o m
© 2014 Stirling Dynamics