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Power Matters
Applying a System View to Align Efficient Multi-device Product Development
Jim Aralis Chief Technology Officer Microsemi November 1, 2012
Power Matters
System view of space products System view driving space roadmaps
Where these roadmaps lead?
• New at corporate Microsemi • New products and technologies
Summary
Agenda
© 2012 Microsemi Corporation. CONFIDENTIAL 2
Power Matters
System view of space products
Power Matters
System engineers always look at a satellite as a system
Interfaces and partitioning are done at this level of engineering
Without coordination of component development • Difficult and limited choices in partitions • Performance, power, weight, and cost are sacrificed • Interoperability assurance diminished
System View Device Development
© 2012 Microsemi Corporation. CONFIDENTIAL 4
Power Matters
If the device designers look at the system design to define products • Digital interface formats aligned • Digital and analog physical interfaces aligned • Power generation optimized for load and rails • No more “level converters”, “signal dividers”, extra clock channels, … • Product introductions aligned • Reliability architected into the component systems
System View Device Development
© 2012 Microsemi Corporation. CONFIDENTIAL 5
Power Matters
To take advantage of this advanced view of product definition
• Companies can align products in their portfolio • Companies can partner • General standards
System View Device Development
© 2012 Microsemi Corporation. CONFIDENTIAL 6
Size, power, cost, performance optimization
Power Matters
Examples • High speed digital interfaces, standard, and custom • Analog converters (A/D, D/A) dynamic range alignment • Integrated voltage and current references • POL devices and FPGA or ASIC current and voltage load matching • Consistent cross device radiation performance (weakest link) • High temperature switching device drivers optimized to switching device
characteristics • Serial communication width appropriate for the device technologies involved • FPGA’s control and monitoring clock and power generation. • Optimized device power down.
System View Device Development
© 2012 Microsemi Corporation. CONFIDENTIAL 7
VCC
+5V dc
+3.3V dc
+1.5V dc
Power Matters
System view driving space roadmaps
Power Matters
Solar Array
Satellite Block Diagram
Telemetry Tracking &
Control
Command & Data
Handling
Electronic Power System
Attitude & Orbit
Control
Payload Interface
Unit
Star / Sun Sensors
Magnetometer
Torque Rods
Receive Antenna
Transmit Antenna
Bus / Platform
Payload Power
Conditioning
RF Repeater (“Bent Pipe”)
Remote Sensing Payload
Digital Communications
Payload
Payload
Main Power Bus
© 2012 Microsemi Corporation. 9
Power Matters
Next generation RT FPGA’s • High speed communications common with our space system managers • POL matched to load requirements, programmable and monitoring
Space system companion devices • Analog and/or digital processing • “Custom ASIC” • High speed interfaces • Digital bus alignment
High power switching devices
• Custom drivers for optimized performance and protection • Device switching constraints eliminated from user Systems design teams needs built into roadmaps
Roadmap alignment
© 2012 Microsemi Corporation. 10
Power Matters
Where these roadmaps lead
Power Matters
MSCC: Where these roadmaps lead
New at corporate Microsemi
© 2012 Microsemi Corporation. CONFIDENTIAL 12
Power Matters
About Microsemi
Focused on Providing Solutions Where Power Matters, Security is Non-negotiable, & Reliability is Vital
Defense & Security Space & Aerospace Enterprise & Communications Industrial & Alternative Energy
Industry's Most Extensive Technology Portfolio for Targeted Markets
High-performance, High-reliability Analog Devices Mixed-signal & RF Integrated Circuits Customizable System on Chip Solutions (Analog + FPGA + uController) Complete Subsystems
13 © 2012 Microsemi Corporation.
Power Matters
A Global Footprint
14
Manila, Philippines
Hod Hasharon, Israel
Shanghai, China
Bordeaux, France
Ennis & Dublin Ireland
Lowell, MA Lawrence , MA
Bend, OR
Santa Clara, CA Folsom, CA
Mt. View, CA
Aliso Viejo, CA (HQ) Garden Grove, CA
Irvine, CA
Phoenix, AZ
Lake Mary, FL Hyderabad, India
W. Lafayette, IN
Caldicott, UK
Ottawa, Canada
Austin, TX
San Diego, CA
Singapore
Reading, PA
Power Matters
MSCC: Where these roadmaps lead
New products and technologies
© 2012 Microsemi Corporation. CONFIDENTIAL 15
Power Matters
Efficient Solar Panel Conversion
16 © 2012 Microsemi Corporation
MSCC is enhancing system efficiency by direct conversion from the Solar Panel • Typically 100 v to 120 v • Instead of 100 v to 28 v @ 75% and then from 28 v to 3.3 v @ 75% efficiency, the SA50-120 converts from 120 v to
3.3 v @ 86%.
Soon to be released SB30-100 family will provide lower power system requirements SA50 and SB30 families interface directly with switching and linear MSCC POLs to
provide total system power requirements
Power Matters
RH BiPolar Junction Transistors
17 © 2012 Microsemi Corporation
TID Characterization New JANSR RadHard Slash Sheets ELDRS Characterization
2N2222A Radiation Matrix Mean hFE@Vce=10V vs Ic (07-17-03)Lot 1775-18 Standard Nitride, RAD=57RAD(Si)/s, Vce Bias=45V
1
10
100
1000
1.E-06 1.E-05 1.E-04 1.E-03 1.E-02 1.E-01 1.E+00
Ic (A)
Mea
n hF
E
300k100k30k10k3kControlSpec MinSpec MaxPost R-Rad (100k) Min
1
10
100
1000
0.00001 0.0001 0.001 0.01 0.1 1Collector Current (A)
Mea
n hF
E (1
0pcs
)
0k3k10k30k100k300k1000kSpec MinSpec MaxPost R-Rad (100k) MinPost R-Rad (1000k) Min
Level 2 IPG 2N2222A RH1 Lot E420002 Vce Bias=60VSpecial Photomask, Special CVD, Gamma 97RAD(Si)/s Tested 08-05-04
Power Matters
RH BiPolar Junction Transistors
18 © 2012 Microsemi Corporation
TID Characterization New JANSR RadHard Slash Sheets ELDRS Characterization
BVCEO IC Pol DIE Redesign New "S" Add RHA RAD Qual RADSS (V) (A) Type SIZE Pkg Review If Needed Qual /Sheet Submit QPL
JANSH 2N2222A /255 50 V 0.8 A NPN 23x23 TO-18, UB, UA X X X X X XJANSF 2N2369A /317 15 V 0.1 A NPN 20x20 TO-18, UB, UA X N/A N/A X X XJANSR 2N2907A /291 60 V 0.8 A PNP 23x23 TO-18, UB, UA X X 1/ X X XJANSR 2N2920 /355 60 V 0.03 A NPN 15x19 TO-78, LCC6 X X 2/ X JANSR 2N2484 /376 60 V 0.05 A NPN 15x19 TO-18, UB, UA X X 2/ X JANSR 2N3439 /368 350 V 1 A NPN 49x57 TO-39, U4 X X X X X XJANSR 2N3501 /366 150 V 0.3 A NPN 24x26 TO-39, UB, U4 X X X X X XJANSR 2N3637 /357 175 V 1 A PNP 24x26 TO-39, UB X N/A N/A X X XJANSR 2N3700 /391 80 V 1 A NPN 24x26 TO-18, UB X X X X X XJANSR 2N5153 /545 80 V 2 A PNP 128x128 TO-39, U3 X N/A N/A X X XJANSF 2N5154 /544 80 V 2 A NPN 120x120 TO-39, U3 X X X X X XJANSR 2N3019 /391 80 V 1 A NPN 24x26 TO-39 X X X X X XJANSR 2N5237 /394 120 V 10 A NPN 128x128 TO-39 X X X X JANSR 2N5238 /394 170 V 10 A NPN 128x128 TO-39 X X X X JANSR 2N5666 /455 200 V 5 A NPN 128x128 TO-39, U3 X X 2/ X JANSR 2N5667 /455 300 V 5 A NPN 128x128 TO-39, U3 X X 2/ X JANSR 2N3765 /396 60 V 1.5 A PNP 40x40 TO-46, U3 X N/A 2/ XJANSF 2N5004 /534 80 V 10 A NPN 128x128 TO-59 Iso X X X X X XJANSR 2N5664 /455 200 V 5 A NPN 128x128 TO-66 X X 2/ X JANSR 2N2219A /251 30 V 0.8 A NPN 23x23 TO-39 X X X X X XJANSR 2N3810 /336 60 V 0.05 A PNP 15x19 TO-78, LCC6 X X X X X XJANSF 2N7373 /613 80 V 5 A NPN 120x120 TO-254 X N/A X X X X
RAD-HardPart Number
1/ Redesign in-process to boost Radiation Hardness beyond Level R (100K)2/ Redesign in-process for initial Radiation Hardened Qualification.
Power Matters
RH BiPolar Junction Transistors
19 © 2012 Microsemi Corporation
TID Characterization New JANSR RadHard Slash Sheets ELDRS Characterization
•Dose rate: .01 Rad(s)/ sec. (10 mrads)
•Test facility: Umass- Lowell •Co- 60 Source •TID, Proton, ELDRS •DLA Certified Facility
•Products Tested to Date (Reports available) •2N2222A •2N2907A •2N3700 •2N2369
•Custom Radiation testing
Power Matters
GaN for Space and High Rel
20 © 2012 Microsemi Corporation
Microsemi has partnered for the development of Space and High Rel GaN products
Superior alternative to today's existing hermetic MOSFETs. 40V to 200V Surface Mount Packages Leaded Packages “Flip Chip” Bumped Die
• Ultra small footprint • Ultra efficient
G
S S S S D D D D
- Honored with an Electronics Products Magazine Product of the Year Award
PART NO. VOLTAGE CURRENT PEAK RDS(ON) (mΩ)
Date available
MGN2915U4A 40V 33A 150A 4 Mid- October-’12
MGN2905U4A 60V 25A 100A 7 TBD MGN2901U4A 100V 25A 100A 7 Nov- ‘12 MGN2911U4A 150V 12A 40A 25 TBD MGN2910U4A 200V 12A 40A 25 TBD
U4A U4A
Power Matters
GaN for Space and High Rel
21 © 2012 Microsemi Corporation
Normalized Rds(on) is lower than Si: 1.47 vs. 1.7
Natural Logic- Level drive • +5V gate drive- fully enhanced at +4.5V • Vgsmax= 6.5V!!!
Small die size will result in much smaller packages
• Custom packages in development • Standard HiRel packages also will be available
Radiation resistant HiRel products in Development
• Heavy Ion testing in progress • TID, ELDRS characterization
Extremely low parasitic capacitance
• Cuts switching losses by at least 50% • High frequency operation results in higher density power designs
Power Matters 22
Solid- State Relays Features
• MIL-PRF- 38534 • Accepts Logic Level inputs, (+3.0V- +5.5V) • 1A, 5A & 10A Max Current • Class H & K Screening levels • Surface Mount & Thru- Hole packages • Normally open or Normally closed operation
Applications Heater controls Launch Systems- explosive bolts Solar panel power control
Part # Description Rated Switch Voltage
Status
MHS2005 Dual, 5A Relay 200V Protos in assy. Flight material ordered
MHS1005 Dual, 5A Relay 100V Proto material in- house Protos: ; Flight:
MHS1010 Dual, 10A 100V Proto material in- house Protos: ; Flight:
MHS0620 Single 20A 60V In design
MHS2010 Dual 20A 200V In design
© 2012 Microsemi Corporation. 22
Power Matters
RTAX-DSP: Architecture Overview
•Builds upon established RTAX-S/SL architecture •QML qualification expected 2012 •Hardened by Design •SET Hardened
•R-Cell 16X improvement •Math BLock < 5E-9 Error/DSP bit/day
23 © 2012 Microsemi Corporation..
Power Matters
Next Generation Space-Flight FPGAs
Block RAM (18Kb)
Mathblocks
µRAM (1Kb)
PLL
Logic SERDES
SDRAM DDR Controller
© 2011 Microsemi Corporation. 24
X
D
EN
>> 17
C[43:0]
SHIFT17
SEL_CASC
SN[43:0]
OVFL / CO
ADD_SUBA[17:0]
B[17:0] +
SN-1[43:0]
D[43:0]
Fracturable Logic Module with SEU-protected Flip Flop,
300 MHz operation
Multiply-Accumulate Block with SEU and SET protection,
300 MHz operation
High performance, low power 65nm process Radiation hardened by design 300MHz in-system performance Embedded hardened SERDES, LVDS,
SRAM, PLL, Spacewire, . . . Flight units qualified in 2015
Power Matters
Features: • 700mA per output source current • 3.5X the current of the IS-2981RH so no need to parallel outputs for higher current capability • Fully isolated channels with DI process • 100krad TID, SEL immune • 80V minimum output breakdown • Low quiescent current consumption • Internal ground clamp diodes • Internal thermal shutdown • TTL, 5V, and 12V logic compatible • AAHS298A with Over-current protection will be available in Q4
Target Markets: • Aerospace satellite manufacturers • Military power electronics control
Applications: • Can be used as High-Voltage drivers for Lamps, Relays, Solenoids and Motors • Recommended for high-side switching applications that benefit from separate logic and load grounds. • Reliable Replacement of Discrete Solutions • Interfacing Between Low-Level Logic and High-Current Loads • For high reliability application, it can be used for Redundant Power Distribution
© 2012 Microsemi Corporation. 25
AAHS298B – 8 Channel Source Driver
Power Matters
Summary
Microsemi remains Focused on Space
We are investing in new processes, devices, and products driven by system partitioning and interoperability. (System Look) We do this both in internal R&D and in our acquisition strategy.
We continue to have one of broadest and most diverse product
and capabilities space portfolios in the world.
Recent additions to our space offering is significant in many areas.
We will be here when you need us in twenty years and more …
© 2012 Microsemi Corporation. 26
Power Matters
Thank you !