LORAN-C Band Data Collection Efforts at Ohio University Presented by Curtis Cutright to the International LORAN Association 32nd Annual Convention and Technical Symposium Boulder, CO November 6, 2003
Download ReportTranscript LORAN-C Band Data Collection Efforts at Ohio University Presented by Curtis Cutright to the International LORAN Association 32nd Annual Convention and Technical Symposium Boulder, CO November 6, 2003
Slide 1
LORAN-C Band Data
Collection Efforts at
Ohio University
Presented by Curtis Cutright
to the International LORAN Association
32nd Annual Convention and
Technical Symposium
Boulder, CO
November 6, 2003
Slide 2
Outline
• Task overview
• Data collection system overview
– Airborne data collection equipment
– Lab data collection equipment
– Initial data collection results
• Task progress
Ohio University • Avionics Engineering Center
Slide 3
Task
• Field a data collection system capable of digitizing
storing atmospheric noise for subsequent analysis
• Integrate this system into an airborne flight platform
• Perform data collection under varying atmospheric
conditions
Ohio University • Avionics Engineering Center
Slide 4
Purpose
•
Develop threat models for aircraft in flight
•
Precipitation static (p-static)
•
Atmospheric noise
• Man-made noise(cross rate, CW)
• Lightning
Ohio University • Avionics Engineering Center
Slide 5
Purpose
• Identify all trade-off’s for E and H-field antennas,
SNR, phase error, saturation, bandwidth
Ohio University • Avionics Engineering Center
Slide 6
To be determined
•
Is ground-based noise the same as airborne
noise(E-field and H-field)
• Aircraft man-made noise
•
CW interference environment
•
Determine actual P-static mechanism
•
Phenomena under thunderstorms
• Antenna and pre-amp performance
Ohio University • Avionics Engineering Center
Slide 7
Data Collection
• Simultaneous ground and aircraft RF data
collection (Using DataGrabber)
• 2 channels, 16-bits samples, 400 kSamples/s
• LORAN receivers for performance assessment
• GPS WAAS for position reference
Ohio University • Avionics Engineering Center
Slide 8
Data Processing
• P-Static
• Characterize E-field and H-field antenna
performance
• Compare measured lightning noise with predicted noise
based on the national lightning detection
network(NLDN)
• Compare ground and airborne noise
• Compare airborne E-field and H-field noise
Ohio University • Avionics Engineering Center
Slide 9
Data Collection System
Overview
Slide 10
Airborne Data Collection Equipment
•
Aircraft
– King Air C-90B
– Pressurized twin turboprop
– 240 knot cruise speed
•
Equipment
– Novatel OEM4 GPS
receiver
– LORADD-DS DataGrabber
– WX-500 StormScope
– Apollo 618
– Data collection PC
Ohio University • Avionics Engineering Center
Slide 11
Whip antenna
GPS antenna
(e-field)
Apollo 618
Data Collection PC
Data
Collection
Equipment
WX-500 StormScope
Pre-amp
ADF antenna
Stormscope
(h-field)
antenna
Ohio University • Avionics Engineering Center
Slide 12
Data Collection PC
• CyberResearch dual backplane with 933MHz P-III CPU
cards
• 512MB RAM
• 160GB of hard-drive space
Ohio University • Avionics Engineering Center
Slide 13
WX-500 Stormscope
• RS-232 data output
• 200nmi range
• Heading stabilization
• Data will be used in conjunction with National Lightning
Detection Network (NLDN) data
Ohio University • Avionics Engineering Center
Slide 14
Loran-C H-Field vs. E-Field Antennas
E-Field
(Electric)
•
Large effective height
– Little voltage amplification
needed
•
High impedance (MW)
– Charge build-up (cannot be
terminated)
•
Antenna phase pattern is
omnidirectional
•
Whip or wire antenna
H-Field
(Magnetic)
• Small effective height
Large voltage
amplification needed (low
noise pre-amp)
• Low impedance (1W)
No charge build-up
(antenna is grounded)
• One loop creates 0 and 180
degrees.
• Conformal antenna
Ohio University • Avionics Engineering Center
Slide 15
Aircraft Data Collection Equipment
Ohio University • Avionics Engineering Center
Slide 16
Antennas
E-Field
II Morrow A-16
H-Field
King Radio KA42A
Ohio University • Avionics Engineering Center
Slide 17
Rackmount chassis for data collection equipment
AC in
DC Power
Supply
LORADD-DS
DataGrabber
GPS
Novatel GPS
Receiver
GPS
antenna
LAN
Antenna
Antenna
Interface
Interface
H-field
E-field
Ohio University • Avionics Engineering Center
Slide 18
LORADD-DS DataGrabber
• Sampling rate: 400kHz
• Resolution: 16 bits
• Dynamic range: 96dB
• Two input channels – sampled simultaneously
• Differential input amplifiers for the antennas
• TCP/IP data output
• Clock stability: 1ppm
Ohio University • Avionics Engineering Center
Slide 19
Antenna Interface Boxes
• Adjust received signal level
• Provide interference isolation for the antenna cable
• Impedance matching for the DataGrabber antenna
inputs
Ohio University • Avionics Engineering Center
Slide 20
Novatel GPS Receiver
• 1-20 Hz position data
• Time synchronization
• RS-232 data output (ASCII or binary)
Ohio University • Avionics Engineering Center
Slide 21
Lab Data Collection Equipment
• LORADD-DS
DataGrabber
– 400kHz sampling
– Dual channel
• Data collection PC
Ohio University • Avionics Engineering Center
Slide 22
Antennas
• E-field
– IIMorrow A-16 Whip
antenna with integral
preamplifier/impedance
transformer
– Powered by an Apollo 618
LORAN receiver
Ohio University • Avionics Engineering Center
Slide 23
Antennas
• H-field
– King KA42A ADF Loop
antenna
– Requires a separate
preamplifier/impedance
transformer tuned to the
LORAN-C band
– Powered by 5-10VDC
Ohio University • Avionics Engineering Center
Slide 24
Initial Data Collection Results
•
The next 2 slides show screen captures from the initial lab data
collection test using both antennas
•
Channel 1: h-field
•
Screen capture 1 shows the RF data from each antenna
Channel 2: e-field
– The presence of the LORAN signal can be seen in each channel
– E-field channel (bottom) has more amplification than h-field (this
does not affect the SNR)
•
Screen capture 2 shows the spectrum of the RF data
– The filter bandwidth around 100kHz is apparent
– Several CW interference sources are evident
Ohio University • Avionics Engineering Center
Slide 25
Ohio University • Avionics Engineering Center
Slide 26
Example of collected data: Time domain
Ohio University • Avionics Engineering Center
Slide 27
Ohio University • Avionics Engineering Center
Slide 28
Example of collected data: Spectrum
Ohio University • Avionics Engineering Center
Slide 29
Current Status of the Data
Collection Task
Slide 30
Airborne Collected Data
• “Clear” – 10hrs
• Overcast – 4hrs
• Close t-storm (<20nmi) – 20min
• Nearby t-storm – 2hrs
• Other – 4+hrs
Ohio University • Avionics Engineering Center
Slide 31
Data Collection Flight Tracks
Ohio University • Avionics Engineering Center
Slide 32
Thunderstorm Data Conditions
Ohio University • Avionics Engineering Center
Slide 33
Ohio University • Avionics Engineering Center
Slide 34
Ohio University • Avionics Engineering Center
Slide 35
Future Work
• Continue data collection effort
– Varying environmental conditions
– Different locations
– Correlate National Lightning Detection Network
(NLDN) data
– Mobile ground data collection equipment
• Calibrate the DataGrabber
• Aircraft noise analysis
Ohio University • Avionics Engineering Center
Slide 36
Acknowledgements
• Mitch Narins (FAA)
• Wouter Pelgrum (Reelektronika)
• Bryan Branham (Ohio University)
• Jay Clark (Ohio University)
Ohio University • Avionics Engineering Center
Slide 37
Questions?
LORAN-C Band Data
Collection Efforts at
Ohio University
Presented by Curtis Cutright
to the International LORAN Association
32nd Annual Convention and
Technical Symposium
Boulder, CO
November 6, 2003
Slide 2
Outline
• Task overview
• Data collection system overview
– Airborne data collection equipment
– Lab data collection equipment
– Initial data collection results
• Task progress
Ohio University • Avionics Engineering Center
Slide 3
Task
• Field a data collection system capable of digitizing
storing atmospheric noise for subsequent analysis
• Integrate this system into an airborne flight platform
• Perform data collection under varying atmospheric
conditions
Ohio University • Avionics Engineering Center
Slide 4
Purpose
•
Develop threat models for aircraft in flight
•
Precipitation static (p-static)
•
Atmospheric noise
• Man-made noise(cross rate, CW)
• Lightning
Ohio University • Avionics Engineering Center
Slide 5
Purpose
• Identify all trade-off’s for E and H-field antennas,
SNR, phase error, saturation, bandwidth
Ohio University • Avionics Engineering Center
Slide 6
To be determined
•
Is ground-based noise the same as airborne
noise(E-field and H-field)
• Aircraft man-made noise
•
CW interference environment
•
Determine actual P-static mechanism
•
Phenomena under thunderstorms
• Antenna and pre-amp performance
Ohio University • Avionics Engineering Center
Slide 7
Data Collection
• Simultaneous ground and aircraft RF data
collection (Using DataGrabber)
• 2 channels, 16-bits samples, 400 kSamples/s
• LORAN receivers for performance assessment
• GPS WAAS for position reference
Ohio University • Avionics Engineering Center
Slide 8
Data Processing
• P-Static
• Characterize E-field and H-field antenna
performance
• Compare measured lightning noise with predicted noise
based on the national lightning detection
network(NLDN)
• Compare ground and airborne noise
• Compare airborne E-field and H-field noise
Ohio University • Avionics Engineering Center
Slide 9
Data Collection System
Overview
Slide 10
Airborne Data Collection Equipment
•
Aircraft
– King Air C-90B
– Pressurized twin turboprop
– 240 knot cruise speed
•
Equipment
– Novatel OEM4 GPS
receiver
– LORADD-DS DataGrabber
– WX-500 StormScope
– Apollo 618
– Data collection PC
Ohio University • Avionics Engineering Center
Slide 11
Whip antenna
GPS antenna
(e-field)
Apollo 618
Data Collection PC
Data
Collection
Equipment
WX-500 StormScope
Pre-amp
ADF antenna
Stormscope
(h-field)
antenna
Ohio University • Avionics Engineering Center
Slide 12
Data Collection PC
• CyberResearch dual backplane with 933MHz P-III CPU
cards
• 512MB RAM
• 160GB of hard-drive space
Ohio University • Avionics Engineering Center
Slide 13
WX-500 Stormscope
• RS-232 data output
• 200nmi range
• Heading stabilization
• Data will be used in conjunction with National Lightning
Detection Network (NLDN) data
Ohio University • Avionics Engineering Center
Slide 14
Loran-C H-Field vs. E-Field Antennas
E-Field
(Electric)
•
Large effective height
– Little voltage amplification
needed
•
High impedance (MW)
– Charge build-up (cannot be
terminated)
•
Antenna phase pattern is
omnidirectional
•
Whip or wire antenna
H-Field
(Magnetic)
• Small effective height
Large voltage
amplification needed (low
noise pre-amp)
• Low impedance (1W)
No charge build-up
(antenna is grounded)
• One loop creates 0 and 180
degrees.
• Conformal antenna
Ohio University • Avionics Engineering Center
Slide 15
Aircraft Data Collection Equipment
Ohio University • Avionics Engineering Center
Slide 16
Antennas
E-Field
II Morrow A-16
H-Field
King Radio KA42A
Ohio University • Avionics Engineering Center
Slide 17
Rackmount chassis for data collection equipment
AC in
DC Power
Supply
LORADD-DS
DataGrabber
GPS
Novatel GPS
Receiver
GPS
antenna
LAN
Antenna
Antenna
Interface
Interface
H-field
E-field
Ohio University • Avionics Engineering Center
Slide 18
LORADD-DS DataGrabber
• Sampling rate: 400kHz
• Resolution: 16 bits
• Dynamic range: 96dB
• Two input channels – sampled simultaneously
• Differential input amplifiers for the antennas
• TCP/IP data output
• Clock stability: 1ppm
Ohio University • Avionics Engineering Center
Slide 19
Antenna Interface Boxes
• Adjust received signal level
• Provide interference isolation for the antenna cable
• Impedance matching for the DataGrabber antenna
inputs
Ohio University • Avionics Engineering Center
Slide 20
Novatel GPS Receiver
• 1-20 Hz position data
• Time synchronization
• RS-232 data output (ASCII or binary)
Ohio University • Avionics Engineering Center
Slide 21
Lab Data Collection Equipment
• LORADD-DS
DataGrabber
– 400kHz sampling
– Dual channel
• Data collection PC
Ohio University • Avionics Engineering Center
Slide 22
Antennas
• E-field
– IIMorrow A-16 Whip
antenna with integral
preamplifier/impedance
transformer
– Powered by an Apollo 618
LORAN receiver
Ohio University • Avionics Engineering Center
Slide 23
Antennas
• H-field
– King KA42A ADF Loop
antenna
– Requires a separate
preamplifier/impedance
transformer tuned to the
LORAN-C band
– Powered by 5-10VDC
Ohio University • Avionics Engineering Center
Slide 24
Initial Data Collection Results
•
The next 2 slides show screen captures from the initial lab data
collection test using both antennas
•
Channel 1: h-field
•
Screen capture 1 shows the RF data from each antenna
Channel 2: e-field
– The presence of the LORAN signal can be seen in each channel
– E-field channel (bottom) has more amplification than h-field (this
does not affect the SNR)
•
Screen capture 2 shows the spectrum of the RF data
– The filter bandwidth around 100kHz is apparent
– Several CW interference sources are evident
Ohio University • Avionics Engineering Center
Slide 25
Ohio University • Avionics Engineering Center
Slide 26
Example of collected data: Time domain
Ohio University • Avionics Engineering Center
Slide 27
Ohio University • Avionics Engineering Center
Slide 28
Example of collected data: Spectrum
Ohio University • Avionics Engineering Center
Slide 29
Current Status of the Data
Collection Task
Slide 30
Airborne Collected Data
• “Clear” – 10hrs
• Overcast – 4hrs
• Close t-storm (<20nmi) – 20min
• Nearby t-storm – 2hrs
• Other – 4+hrs
Ohio University • Avionics Engineering Center
Slide 31
Data Collection Flight Tracks
Ohio University • Avionics Engineering Center
Slide 32
Thunderstorm Data Conditions
Ohio University • Avionics Engineering Center
Slide 33
Ohio University • Avionics Engineering Center
Slide 34
Ohio University • Avionics Engineering Center
Slide 35
Future Work
• Continue data collection effort
– Varying environmental conditions
– Different locations
– Correlate National Lightning Detection Network
(NLDN) data
– Mobile ground data collection equipment
• Calibrate the DataGrabber
• Aircraft noise analysis
Ohio University • Avionics Engineering Center
Slide 36
Acknowledgements
• Mitch Narins (FAA)
• Wouter Pelgrum (Reelektronika)
• Bryan Branham (Ohio University)
• Jay Clark (Ohio University)
Ohio University • Avionics Engineering Center
Slide 37
Questions?