Summer Tasks on UAV Radar Under supervision of: Shannon Rodríguez Lihua Li Gerry Heymsfield Manuel A. Vega-Cartagena UPRM Graduate Student Goddard Space Flight Center
Feb 12, 2016
Summer Tasks on UAV Radar
Under supervision of:Shannon RodríguezLihua LiGerry Heymsfield
Manuel A. Vega-CartagenaUPRM Graduate Student
Goddard Space Flight Center
Manuel A. Vega-Cartagena2
Objective
NASA IDEAS-ER grant received.
Develop a background on radar design while contributing to the UAV project.
Manuel A. Vega-Cartagena3
UAV Radar Project
The planned radar will have capabilities of ER-2 Doppler Radar (EDOP).
Nadir beam for vertical winds and precipitation structure.
Conical beam for ocean surface winds and surveillance of the precipitation regions of the storm.
Manuel A. Vega-Cartagena4
Tasks
Study radar literature.
Redesign UAV’s nadir sub-system RF front end block diagram.
Help bench test UAV’s conical sub-system Tx and Rx paths.
Design 80MHz/5MHz clock PCB.
Design a PCB for UAV’s Vicor power modules.
Manuel A. Vega-Cartagena5
UAV’s RF Front End Block Diagram
Requirements
– Magnetron frequency = 9.345 GHz
– Intermediate frequency = 60 MHz
– Calibration noise injection loop
– Receiver noise figure calculations
Manuel A. Vega-Cartagena7
80MHz / 5MHz PCB
Requirements
– Single 10MHz sine wave input.
– 80MHz and 5MHz TTL clock outputs for DAQ card.
– Four amplified analog sensing lines.
– Low profile components.
– PMC daughter card format.
– Original circuit design done by Shannon Rodríguez.
Manuel A. Vega-Cartagena8
80MHz / 5MHz PCB
5V
-5V
Frequency MultiplierAV9170
10 MHz10 MHz 40 MHz
Clock Block Diagram:
Manuel A. Vega-Cartagena9
80MHz / 5MHz PCB
PCB Construction– Board schematic and layout
done with Orcad software.– Built using router in building 22.
MezzanineConnectors
SOICComponents
D-Sub 15Sense Lines
Manuel A. Vega-Cartagena10
80MHz / 5MHz PCB
Board Testing– CPCISYS carrier board with daughter card.– Only DC Power from carrier board used.– Still undergoing debugging process.
Manuel A. Vega-Cartagena11
80MHz / 5MHz PCB
Test Results– 80MHz Clock Signal
80MHz TTL Clock Signal
0
0.2
0.4
0.6
0.8
1
1.2
1.4
1.6
-1.50E-07 -1.00E-07 -5.00E-08 0.00E+00 5.00E-08 1.00E-07 1.50E-07
Time (s)
Volta
ge (V
)
~1.3V
~0.4V
Manuel A. Vega-Cartagena12
80MHz / 5MHz PCB
5MHZ Clock Signal SMA5MHz TTL Clock Signal
0
0.2
0.4
0.6
0.8
1
1.2
1.4
1.6
1.8
2
-5.00E-07 -4.00E-07 -3.00E-07 -2.00E-07 -1.00E-07 0.00E+00 1.00E-07 2.00E-07 3.00E-07 4.00E-07 5.00E-07
Time (s)
Volta
ge (V
)
~1.6V
~0.1V
Manuel A. Vega-Cartagena13
80MHz / 5MHz PCB
Sensing Lines– Two additional lines were added.– Two inverting amplifier stages.– Gain values were changed.
3
21
411
-
+
U1A
LM324/SO
5
67
411
-
+
U2B
LM324/SO
0 0
R1
R
R2
R
R3
R
R4
R
VinVout
Manuel A. Vega-Cartagena14
80MHz / 5MHz PCB
Sense Lines– Tested using 10Vpp 1kHz
sine wave.
– Theoretical voltage gain value = 2.25.
– Gain variations may be caused by tolerance in resistances.
Sense LineOutput Voltage (Vpp)
Voltage Gain
1 19.53 1.953
2 20.31 2.031
3 19.53 1.953
4 19.53 1.953
Manuel A. Vega-Cartagena15
Vicor Power Modules PCB
Requirements– Eliminate wire connections
between modules.
– Reduce mounting time.
– Only one board for both +/- voltage configurations.
– Output voltages should be accessible and easy to change(+/- 5V, +/-12V, +/-15V).
Manuel A. Vega-Cartagena16
Vicor Power Modules PCB
Design Schematic– Power modules PCB.
Voltage selection jumper and output.
Wire connections elimination.
Bypass capacitors.
Chassis ground connection. 12
J1+28V
12
J2
GND
IN-
Gate
OUT
Gate
IN
IN+
OUT-
OUT+
-S
Trim +S
U1Vicor DC-DC Converter
-IN1
-Sin
2
+Sin
3
+IN
4
-OUT
9
-Sou
t8
NC7
+Sou
t6
+OUT
5
U2VI-RAM-I2
0
To Plate Screw
From Power Distribution Matrix
To Power Distribution Matrix
C1CAP
C2CAP
C3CAP
C4CAP
00
0 0
1 2 3 4
J3+/- OUT
0
Manuel A. Vega-Cartagena17
Vicor Power Modules PCB
PCB Construction– Maximum load currents calculation.
Imax = 5 A @+24VIN for 5V module. 12V and 15V modules have lower output currents. Track widths for 10°C temperature increase = 110 mils. Track clearances for +28V = 29 mils. Entire design done using standard low-cost 1oz. Cu thickness
board.– Components selection.
Connectors with unexposed contacts.
Manuel A. Vega-Cartagena18
Vicor Power Modules PCB
Finished Board
+28V Input
Chassis Ground
Output and VoltageSelection Jumper
Manuel A. Vega-Cartagena19
Vicor Power Modules PCB
Power Distribution Matrix– Used to eliminate barrier
block.– Makes output voltages more
accessible and easy to change.
12
J4+5V
12
J5-5V
12
J6+12V
12
J7-12V
1 2
J8+28V
1 2
J9+28V
1 2
J10+28V
1 2
J11+28V
1 2
J12+28V
To Power Modules
From AircraftFrom Power Modules
0
0
NOTE: All voltages available at each connector.Total Components = 10
To Components
12
34
56
J13CON6A
12
34
56
J14CON6A
12
34
56
J15CON6A
12
34
56
J16CON6A
12
34
56
J17CON6A
From Aircraft
To Power ModulesTo Components
From Power Modules
Manuel A. Vega-Cartagena20
Vicor Power Modules PCB
Finished BoardFrom Aircraft
To Power ModulesFrom PowerModules
To Components
Manuel A. Vega-Cartagena21
Vicor Power Modules PCB
Final Configuration
Manuel A. Vega-Cartagena22
UAV’s Conical Sub-System Tx and Rx Paths Testing
Task performed to gain hands-on experience.
Manuel A. Vega-Cartagena23
Learning Experience
Radar Theory Background– RF Front End Design– Power Requirements
PCB Design– ORCAD– Routing machine
Design Implementation
Manuel A. Vega-Cartagena24
Conclusions
Goals achieved!– 80MHz/5MHz daughter card PCB developed– Power Modules PCB design developed
Gained valuable hands-on experience.
Manuel A. Vega-Cartagena25
Questions
Manuel A. Vega-Cartagena26
List of Acronyms
UAV – Unmanned Air Vehicle IDEAS – Initiative to Develop Education through Astronomy
and Space Science DCAS – Distributed Collaborative Adaptive Sensing PCB – Printed Circuit Board TTL – Transistor-Transistor Logic
Manuel A. Vega-Cartagena27
Acknowledgements
Shannon Rodríguez / 555 Lihua Li / 912 Gerry Heymsfield / 613 Wai Fong / 567 Gerry McIntire / 613