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“Altera FPGA’s in Avionics/Military”
Adrian Fitzgerald
Senior Business Manager EMEA
Military / Aerospace / Government
1
Altera Coverage of Five Domains
6
• EO/IR sensor fusion
• SAR image formation
• Autonomous navigation
• Target recognition / tracking
• DO-254/DO-178
• Fault tolerant design
• AESA radar system
• Radiation tolerance
• MIL 38535
• Missile guidance
• Motor control
• Kalman filter
• Data analytics
• Data compression
• Data transport
• Signal processor
• Data processor
• Beamforming
• Target detection & location
• EW jammer / receiver
7
Complete Solutions from Altera
Superior Perf / PWR, Security & Reliability
Low-power Hard Floating
Point
SERDES
SiP
Better Component Solutions
Better Systems, Best TCO
Analog
Processing
Digital Processing (FPGA)
Receiver &
MixerBeamforming De-interleaving (sort) Signals
Pa
ssiv
e S
ca
nn
ing
Ultra
-Wid
eb
an
d (
UW
B)
Measurements
AOA, Freq, PRI, Pulse Width,
Power, Etc.
Determine Signal
Type & Char
Determine
Location
Correlate
(Thread ID)
ELINT DB
(Location)Thread UDF DB
(Type)
Ambiguity
Resolution
Track File
Mgmt
Record
Results
Display
Counter Measures
Take Direct
CM Action
Jammer
Chaff
Other
Digital Processing (Altera FPGA)
Signal Analyser
Database
Digital
BeamformingChannelizer
Target
Correlator
Mission Computer /
Operational Control
RF Data Link
Mission Data Loader
Local Algorithm
Storage
Target / Threat
Analysis
Window FFT
Signal Detection /
Freq. Estimation
RF Data
Recording
Weapon Store
Multi-Control Display
Analog
Processing
Receiver &
Mixer
Transmitter &
Mixer
Digital Processing (FPGA)
q
TRM
TRM
TRM
TRM
...
TRM Digital WFG
Target Detection
(CFAR)
Doppler
Processing (MTI)
Pulse
Compression
STAP
Summation Pre-
detect
Signal Processor
Beam
Weights
System Control
Acceleration &
Bridging
Fusion,
Compensation,
Decisions
Data ProcessorDBF
DBF
DBF
DBF
DBF
...
Beam
Forming
Network
Signal
Processing
· Control
· Power
· Display
· Communications
Active Tx & Rx
Narrowband
Digital Processing (Altera FPGA)
Encrypted Data
Digital Up
Convert
Digital Down
Convert Modem DSP
General
Purpose
Processing
Waveform
Processing
Direct RF
Gsps
Decrypted Data
Voice DSP
General
Purpose
Processing
Waveform
Processing
Voice Codec
Crypto
Processing
Altera Security Supervisor IP
Design Separation Flow
Logic Lock and Trace Lock (Design Preservation)
Analog
Processing
Receiver &
Mixer
Transmitter &
Mixer
Analog
Processing
Digital Processing (FPGA)
Receiver &
MixerBeamforming Channelizer
Detector
Parameter
Extraction
Tracker
Digital RF
Memory
(DRFM)
Noise Technique
Direct Digital Synthesizer
(DDS)
Technique
Inverse
Channelizer
Transmitter &
MixerBeamforming
Thre
at Id
entific
atio
n &
Jam
Respon
se
Digital Processing (Altera FPGA)
PreprocessingBack Projection
Image Formation
Coherent
Exploration
Non-Coherent
Exploration
Image
Processing
Image
Analysis
Analog
Processing
Receiver &
Mixer
Transmitter &
Mixer
SA
R
EW
-
Ja
mm
er
EW
-
Re
ce
ive
r
Sig
na
l
Inte
llig
en
ce
Ra
da
r -
AE
SA
Se
cu
re
Co
mm
un
ica
tio
n
Ecosystem
Partners
Customers
8
System vs. Component Life-Cycle Comparison
R&D
2 – 4 years
2 Years Typical,
4 Years (automotive
or safety certification)
Active
5 – 10 years
Complete Technical
and Purchasing
Support (COGS)
Phase Out
1 – 3 years
Spare Parts, Repairs,
Migration to New Technology,
EOL Management
Obsolete
ASSP 5 years (typical)
Low Prices,
Consumer
Driven
MCU
7-10 years (typical)
Altera PLD
+15 years (typical)
Lowest TCO,
Off-the-Shelf, Very Wide
Customer Base, Used by
Many Market Segments
ASIC
10 years (typical)
High NRE,
100% Application Specific
OEM Product
Life-Cycle:
Component
Product
Life-Cycle:
t = 0
Low Prices,
Embedded
Driven
Other PLD
8 - 10 years (typical)
Altera Long Term Commitment to Avionics Production Lifecycles
Avionics Certification Challenges
9
Safety Assessment
Process
(ARP 4761 / ED-135)
Aircraft & System Development Processes
(ARP 4754 / ED-79)
Guidelines for IMA
(DO-297 / ED-124)
Hardware Life-Cycle
(DO-254 / ED-80)
Software Life-Cycle
(DO-178C / ED-12C)
System
Design
Information
Function,
Failure, &
Safety
Information
Intended
Aircraft
Function
Reliability – Safety – Security
Reliability Pertains to system quality
Probability to function properly with respect to component failure
Functional safety Safeguarding of a system against hazards
due to faulty and functional interruption that may lead to dangerous failures
Security System security refers to ‘Cyber Security’
Cyber security: technologies and processes to protect IT systems and networks from malicious actions
Common intersection is fault
tolerance
Functional
Safety
Reliability
Fault
Tolerance
Security
Commercial Safety and Reliability Standards
11
Industrial
IEC 61508
HW / SW
Medical
IEC 60601
Machinery
IEC 62061
Power Drive Sys
IEC 61800
Home Appliance
IEC 60730
Automotive
ISO 26262
Safety Instrumented Sys
IEC 61511
ProcessSWHW System
Space
ECSS-Q60-02
Avionics
DO-254
Nuclear
IEC 60987
Railway Systems
IEC 62425
Avionics
DO-178
Avionics - IMA
DO-297
Railway Signaling - SW
IEC 62279
Railway RAMS
IEC 62278 / EN 50126
Nuclear – SW Cat B or C
IEC 62138
Nuclear – SW Cat A
IEC 60880
Aircraft & Sys Dev
ARP 4754
= SEU or radiation effects consideration requirement
Federated Avionics vs. IMA
12
Becoming more software defined architecture
Current new aircraft have mix of LRU and IMA
Embedded processor is inevitable, but Certification authorities have not granted use of embedded multicore
IMA growth depends on usage of embedded multicore processors
Function 1 Function 2 Function N
Application SW
Infrastructure / OS
Processor
I/O
Application SW
Infrastructure / OS
Processor
I/O
Application SW
Infrastructure / OS
Processor
I/O
...
Sensors
Effectors
Sensors
Effectors
Sensors
Effectors
LRU 1 LRU 2 LRU N
Fu
nc
tio
na
l
Inte
rco
nn
ec
tio
ns
...
General
Processing
Module 1
Infrastructure / Partitioned OS
Processors (Multiple Modules)
Unified Network
...
Remote
Interface
Unit (I/O)
Sensors
Effectors
Sensors
Effectors
...
...
Other FunctionsNavigation
Application SW
Communication
Application SW
...
Remote
Interface
Unit (I/O)
General
Processing
Module N
Remote
Interface
Unit (I/O)
Sensors
Effectors
Sensors
Effectors
Function N
Application SW
Function M
Application SW
...
Remote
Interface
Unit (I/O)
Conclusions
13
Future Solutions Depends on Certification
Shift to IMA Approach Based on Economics SOC FPGA going to be at core of this
IMA Enables More Scalability & Functionality Certification for D0178/D0254 will be critical
Altera View - SOC Solution Will Be Core Aspect
Access Our Information
14
Visit our sites
http://www.altera.com
http://www.altera.com/end-markets/military-aerospace/mil-index.html
https://www.altera.com/military-portal (registration required)
https://go.altera.com/extranet2001/solutions/mil_aero/ma-index.html
Contact us: [email protected]
Topics and Collateral Military Brochure
Applications
DO-254/Safety, Security
COTS, DSP, Reference design information
Military Temperature & Leaded Packaging
Event registration
Thank You
15
Please contact [email protected] or [email protected] for extended information
Or
Contact [email protected] for general questions and support