A Low-Volume, Low-Mass, Low-Power UHF ... - ece.k-state.edu · C/TT-505 Microtransceiver – Design...
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2006 IEEE/AIAA Aerospace Conference2006 IEEE/AIAA Aerospace Conference Kuhn, Lay, Kuhn, Lay, GrigorianGrigorianMars Proximity Mars Proximity MicrotransceiverMicrotransceiver
A Low-Volume, Low-Mass, Low-PowerUHF Proximity Micro-Transceiver
for Mars Exploration
William Kuhn1, Norman Lay2, and Edwin Grigorian2
1Kansas State University2Jet Propulsion Laboratory
Funded by NASA / JPL Mars Technology Program (MTP)
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2006 IEEE/AIAA Aerospace Conference2006 IEEE/AIAA Aerospace Conference Kuhn, Lay, Kuhn, Lay, GrigorianGrigorianMars Proximity Mars Proximity MicrotransceiverMicrotransceiver
Existing Transceivers
Source:http://www.cinele.com/505.htm
•Full-duplex, 401.585 MHz tx, 437.1 rx•PSK or FSK modulation•Sensitivity: -124 dBm @8kbps•RF output power 10W•Size: 6.7” x 5.1” x 3.6”•Mass: 2kg•Power: 45W tx, 5W rx
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2006 IEEE/AIAA Aerospace Conference2006 IEEE/AIAA Aerospace Conference Kuhn, Lay, Kuhn, Lay, GrigorianGrigorianMars Proximity Mars Proximity MicrotransceiverMicrotransceiver
Micro-transceiver Overview
A highly-miniaturized, extremely low-mass, low-power UHF transceiver module for aerobots, microrovers, low-mass penetrators and small network landers.
TCXO Digital Baseband/ Control Circuits
RFTransceiverCircuits
Antenna
Microprocessor/ Memory
Sensors/ Actuators
Small/low-mass
(7 - 20 cm whip)
Control/Sleep
Data
Scout Science Electronics
Microtransceiver Electronics
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2006 IEEE/AIAA Aerospace Conference2006 IEEE/AIAA Aerospace Conference Kuhn, Lay, Kuhn, Lay, GrigorianGrigorianMars Proximity Mars Proximity MicrotransceiverMicrotransceiver
Microtransceiver Goals
• Eliminates need for warm-box and shielding, reducing launch costs, etc.
• Produce working prototype to TRL-6, targeting –100C and 100 krad tolerance
• Permits adoption in near-term mission hardware (e.g. 2011 scouts).
• Provide compatibility with Prox-1 communications infrastructure.
• Offers enabling technology for new classes of scouts, including aerobots, balloons, networked micro-rovers…
• Reduced mass/cost on larger scouts with lower data rate requirements and half-duplex operation.
• Reduce mass, volume, and power
SignificanceGoals
0.01 / 0.1 / 1 W10 WPower (RF out)
< 10 cm32000 cm3Volume
0.05 W / .1 to 3 W5 W / 45 WPDC (RX/TX)
< 10 gms (PCB)2000 gmsMass
MicrotransceiverC/TT-505
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– Design employs a two / three chip solution for 10,100 mW / 1 Watt output.
– Off-chip components limited to Commercial Off-the-shelf (COTS) IF filter and TCXO
– Targets subset of Prox-1 protocols (half-duplex, asymmetric data rates)
– Circuits characterized to –100 C to enable operation outside warm-box in some applications
– Employs rad-hard process and digital library.
Optional1W PA
DigitalModemandControlIC
COTSTCXO
COTSBPF
Transmitter
Synthesizer
Receiver
TX data
IF out
Control
Frequency Reference
Status
RF Transceiver Circuits
RFIC
To / From HostMicrocontroller
Top-Level Block Diagram
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2006 IEEE/AIAA Aerospace Conference2006 IEEE/AIAA Aerospace Conference Kuhn, Lay, Kuhn, Lay, GrigorianGrigorianMars Proximity Mars Proximity MicrotransceiverMicrotransceiver
Implementation Techniques
Peregrine Silicon-on-Sapphire “Ultra-Thin Silicon” IC process employed.
– 0.5um (0.25um available)
– Low parasitics => high fT
– No substrate losses/coupling
– Excellent quality inductors
– 6 flavors of FETs
– MiM capacitors
– MOSFET varactors
– Suitable for digital / analog / RF
– Radiation-hardened “FO” flavor available
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2006 IEEE/AIAA Aerospace Conference2006 IEEE/AIAA Aerospace Conference Kuhn, Lay, Kuhn, Lay, GrigorianGrigorianMars Proximity Mars Proximity MicrotransceiverMicrotransceiver
Implementation Techniques
Cryogenic platform developed at K-State for pre-design characterization of COTS parts and IC process components to < –100 C.
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2006 IEEE/AIAA Aerospace Conference2006 IEEE/AIAA Aerospace Conference Kuhn, Lay, Kuhn, Lay, GrigorianGrigorianMars Proximity Mars Proximity MicrotransceiverMicrotransceiver
Low-Temp Test ResultsSample Cryogenic Test Results
Detailed results presented at 6:30pm poster session.SFECS FA00-R0
-50
-45
-40
-35
-30
-25
-20
-15
-10
-5
0
8.2 9.2 10.2 11.2 12.2 13.2
Frequency (MHz)
Am
plitu
de (d
Bm
)
24˚C -110˚C
0
0.002
0.004
0.006
0.008
0.01
0.012
0.014
0 0.5 1 1.5 2 2.5 3 3.5
Vds (V)Id
(A)
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2006 IEEE/AIAA Aerospace Conference2006 IEEE/AIAA Aerospace Conference Kuhn, Lay, Kuhn, Lay, GrigorianGrigorianMars Proximity Mars Proximity MicrotransceiverMicrotransceiver
Gain
IQModulator
Image RejectMixer
400/450 MHzSynthesizer
TempSensor
RSSI
ADC
IQ10mW
PA
100mWPA
P/S
S/PNcountFcountRcount
IdataQdata
PgmLatch
PgmData
PgmClk
Ref
StatOutStatClk
ADCout
ADCclk
AIFout
RFin
MPAout
LPAout
MPAin
TCXOPwr
IFout IFinGround(multiple)
Vdd(multiple)
VCOcoarseTune
Spare
Spare
AIFoutctrl
ModeSelect
LockDet
GainGain
TX
TX
TX
MPAena
ModeSelect
Reg
PwrDn
Tx/Rx-
Stby
1WPAon
RFIC Development
– Proven architectures employed (superhetreceiver and direct modulation transmitter)
– Iterative fabrication runs to test and center designs
– Transmitter employs large size, high-Q inductors to achieve good efficiency
– Receive trades off IP3 and compression performance for low power
– Half-duplex operation allows transmitter and receiver on same die
– IF sampling and companion digital modem IC provides high-quality demodulation
Optional1W PA
DigitalModemandControlIC
COTSTCXO
COTSBPF
Transmitter
Synthesizer
Receiver
T X data
IF out
C on tro l
Frequency Reference
Status
RF Transceiver Circuits
RFIC
To / From HostMicrocontroller
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2006 IEEE/AIAA Aerospace Conference2006 IEEE/AIAA Aerospace Conference Kuhn, Lay, Kuhn, Lay, GrigorianGrigorianMars Proximity Mars Proximity MicrotransceiverMicrotransceiver
Fab 1 Receiver RFIC Circuits Operational
–Integer-N Synthesizer–LNA + TR switch–Image-reject mixer–IF amplifiers–Amplitude detector–1-Bit ADC–Extensive supply filtering–Stand-alone test structures–Probe points
Synthesizer
Mixer andIF Subsystem
Test Structures
Low NoiseAmplifier
SupplyFiltering
Optional1W PA
DigitalModemandControlIC
COTSTCXO
COTSBPF
Transmitter
Synthesizer
Receiver
T X data
IF ou t
C ontro l
Frequency Reference
Status
RF Transceiver Circuits
RFIC
To / From HostMicrocontroller
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2006 IEEE/AIAA Aerospace Conference2006 IEEE/AIAA Aerospace Conference Kuhn, Lay, Kuhn, Lay, GrigorianGrigorianMars Proximity Mars Proximity MicrotransceiverMicrotransceiver
Fab1 Receiver RFIC Testing
Optional1W PA
DigitalModemandControlIC
COTSTCXO
COTSBPF
Transmitter
Synthesizer
Receiver
T X data
IF ou t
C ontro l
Frequency Reference
Status
RF Transceiver Circuits
RFIC
To / From HostMicrocontroller
Fab1 die
Packaged die on PCB
Spectrum of 1-bit ADC output (1.5 ksps QPSK) IF filter output from +25 C to
–100 C with –100 dBmunmodulated carrier.(reference harmonic spur visible to right)
• Fab-1 die includes all major receiver blocks• Successfully tested from RF-in to sampled IF-out• Low temperature testing shows nominal behavior to
–100C with low parametric drift• Identified areas needing improvement in subsequent
fabs to fully meet performance goals:1. Improve LNA gain to achieve system NF spec2. Provide finer tuning steps and reduce spurs
Cryogenic testing of PC board mounted die
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2006 IEEE/AIAA Aerospace Conference2006 IEEE/AIAA Aerospace Conference Kuhn, Lay, Kuhn, Lay, GrigorianGrigorianMars Proximity Mars Proximity MicrotransceiverMicrotransceiver
Fab2 Transmitter Circuits Operational
– Improved synthesizer with dual-modulus prescaler and 3rd-order MASH fractional-N fine tuning
– First-spin design of 10mW and 100 mW PA circuits
– LNA re-spin with 15 dB additional gain to fix system NF issues from fab 1
– Test structures including temperature sensor
Fractional-NSynthesizer
Mixer and pre-IFfilter amplifiers
TestStructuresLow Noise
Amplifier Re-spin
10 mW / 100 mW PAs
Optional1W PA
DigitalModemandControlIC
COTSTCXO
COTSBPF
Transmitter
Synthesizer
Receiver
T X data
IF ou t
C ontro l
Frequency Reference
Status
RF Transceiver Circuits
RFIC
To / From HostMicrocontroller
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2006 IEEE/AIAA Aerospace Conference2006 IEEE/AIAA Aerospace Conference Kuhn, Lay, Kuhn, Lay, GrigorianGrigorianMars Proximity Mars Proximity MicrotransceiverMicrotransceiver
Digital Modem IC Development
Control Electronics•TX/RX mode control•Transceiver I/O•Subsystem Enable/Disable
Control Electronics•TX/RX mode control•Transceiver I/O•Subsystem Enable/Disable
RF Transmit Circuitry
RF Receive Circuitry
RF Transmit Circuitry
RF Receive Circuitry
Microtransceiver Antenna
Multirate Digital Modulator•1 ksps to 4 Msps•BPSK, QPSK•Rate ½ Conv. Code FEC•Scrambling, encoding, etc.
Multirate Digital Modulator•1 ksps to 4 Msps•BPSK, QPSK•Rate ½ Conv. Code FEC•Scrambling, encoding, etc.
Digital Command Receiver•1, 8, . . . ksps PSK demod•Doppler tolerant acquisitionand tracking
Digital Command Receiver•1, 8, . . . ksps PSK demod•Doppler tolerant acquisitionand tracking
Proximity Protocol Functions•Packet Framing•Single packet ARQ statemachine
•Transceiver commandparsing
Proximity Protocol Functions•Packet Framing•Single packet ARQ statemachine
•Transceiver commandparsing
BasebandI & Q
SampledData
Power Supply Enable/Disable(from Control Subsystem)
Mar
scra
ft I/O
and
Tr
ansc
eive
r Con
trol
Power Supply Enable/Disable,
PA Control
Digital Baseband Functions
Optional1W PA
DigitalModemandControlIC
COTSTCXO
COTSBPF
Transmitter
Synthesizer
Receiver
TX data
IF out
Contro l
Frequency Reference
Status
RF Transceiver Circuits
RFIC
To / From HostMicrocontroller
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2006 IEEE/AIAA Aerospace Conference2006 IEEE/AIAA Aerospace Conference Kuhn, Lay, Kuhn, Lay, GrigorianGrigorianMars Proximity Mars Proximity MicrotransceiverMicrotransceiver
Summary
• First prototype RFIC receiver and transmitter circuits are operational and critical demodulator digital circuits have been prototyped in Matlab and Verilog
• Final version will provide TRL6 validation of Prox-1 compatible micro-transceiver with 100X reduction in mass and volume and > 10:1 reduction in power consumption (for low rate applications) relative to existing solutions.
TCXO Digital Baseband/ Control Circuits
RFTransceiverCircuits
Antenna
Microprocessor/ Memory
Sensors/ Actuators
Small/low-mass
(7 - 20 cm whip)
Control/Sleep
Data
Scout Science Electronics
Microtransceiver ElectronicsThis project targets a highly-miniaturized, extremely low-mass, low-power UHF transceiver module for aerobots,microrovers, penetratorsand small network landers.
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2006 IEEE/AIAA Aerospace Conference2006 IEEE/AIAA Aerospace Conference Kuhn, Lay, Kuhn, Lay, GrigorianGrigorianMars Proximity Mars Proximity MicrotransceiverMicrotransceiver
Acknowledgements and Additional Info
• Igor Kuperman, JPL• Dan Nobbe, Peregrine Semiconductor• Yogesh Tugnawat, K-State / Sprint • Xin He, K-State / Philips• Jeongmin Jeon, K-State• Kai Wong, K-State• Mark Hartter, K-State• Evan Cullens, K-State• Keith Kovala, K-State
Project Web Sites:
Acknowledgements:
• www.eece.ksu.edu/research/mars (public)
• www.eece.ksu.edu/research/microtransceiver (private)