j.tim barrett, dr. mike obal, mike aherne, dr. tatiana

1
L-36 Atlas V launch vehicle • Orbit Altitude 470km – 780km Inclination 64 degrees • Date Delivery January 2012 Flight September 2012 World’s largest deployable from a NanoSat and first attempt at ground point tracking Accomplished to date J.Tim Barrett, Dr. Mike Obal, Mike Aherne, Dr. Tatiana Kitchkaylo, Jeff Sachs, Lucy Hoag, Will Bezouska, Craig Ward, Emin Vartanians, Alexader Shim, Siamak Hesar, Eric Teegarden, Rohan Ramadas, Melissa Christensen, Michael Ortega, Melissa Jawaharlal, Omair Rahman, Amit Shah, Anthony Shao, Nate White, John Razzano, Sara Gramling, Rahul Karkhanis, Chunyih Hsu, Dayung Koh, Neha Rathore, Carson Vogt, Erin Fowler, Amparo Romero, Desiree Webster, Xiaodan Wu, Maria Guzman, Amit Shah, Pezhman Zarifian, Andrew Laskowski, Mike Zarem, Michael Martin, Joe Parsons, Sammi Westall, Rafael Nuguid, Josh Fogel and Anubhav Thakur. Aeneas Got Aperture? Aeneas Got Aperture? The Aeneas Mission Space based tag tracking experiment Space implementation of Marine Asset Tag Tracking System (MATTS) by iControl Inc. Bi-directional 2.4GHz comm. link for Wireless Sensor Network Ultra sensitive receiver to communicate with low power, small, earth based sensors System currently uses ground stations ~ 1 mile range from ports Proof-of-concept: Satellite-based receivers for open ocean or cross country iControl data format selected for DHS Secure CorridorsProgram Various Publications: AIAA Space - Caerus Concept to Flight 11 months, SERC Engineering Teaching Hospital, Aeneas Three-Axis Pointing , Doppler-Based TLE Prediction and Correction and Current USU Small Sat Submissions The authors wish to thank: David Barnhart for mission conception and guidance, the Cubesat Program Office for Colony I and access to launch, Prof. Joe Kunc and Maurice Martin at ORS/AFRL, Congresswoman Jane Harman’s office and ISI Executive Office for funding support. Mission Enabler ½ meter deployable parabola Bus: Colony I -USC Enhanced Three axis stabilized for sun and ground tracking ±1.5° pointing accuracy Mems Gyros Sunsensor Deployable Arrays with 22 watts full sun Primary radio 115/248kbps 437.0 MHz spread spectrum radio Secondary radio 1200 baud AFSK AX.25 Beacon @ 437.6 MHz Amateur Band Dual Processor (FSW - C&HD) Payload: 0.5 m Deployable parabolic antenna 18 dbi at 2.4GHz Space based implementation of Marine Asset Tag Tracking System (MATTS) Bi-directional 2.4GHz communication link for Wireless Sensor Network Ultra sensitive receiver to communicate with low power, small, earth based sensors The Colony I Bus Becomes Aeneas World’s first – ½ Meter Deployable Antenna from CubeSat Filed invention disclosures for the device & processes with USC Stevens Institute USC/ISI plans to provide advanced antenna to others Stowed Antenna Link and Plug Link Vespel- .25” dia x 3.5” long #5 heli-coil Rub plug Material TBD Requirements Concepts/Prototype Design/Implementation Deployment Shock – Wyle Labs Anechoic RF – USC UltraLab Closing the Link Required 18 dB gain on SV Mobile Asset Tracking Tag Frame from Stereolith Model Deployment Video Solidworks Rendering Metrology Testing - JPL -90 -80 -70 -60 -50 -40 180 195 200 205 210 215 220 225 230 235 240 245 250 255 260 265 270 275 280 285 290 295 300 305 310 315 320 325 330 335 340 345 350 355 360 5 10 15 20 25 30 35 40 45 50 55 60 65 70 75 80 85 90 95 100 105 110 115 120 125 130 135 140 145 150 155 160 175 step 0 z=0 deg step 0 z=0 deg -90 -80 -70 -60 -50 -40 180 195 200 205 210 215 220 225 230 235 240 245 250 255 260 265 270 275 280 285 290 295 300 305 310 315 320 325 330 335 340 345 350 355 360 5 10 15 20 25 30 35 40 45 50 55 60 65 70 75 80 85 90 95 100 105 110 115 120 125 130 135 140 145 150 155 160 175 Helix Alone Helix Alone Helix alone -55 dBm (l.) with Parabola -40 dBm (r.) yields 15 dBm gain JPL collaboration Mark Thomson Spacecraft Antennas March 2013 Antenna Stowage 10x10x16.5 cm Payload Bay Hand wound Bifilar Tx & RX Helix(es) and test board Field RF Testing Los Angeles Basin -20 Miles Malibu to Playa Del Rey ground station iGate Receiver and sector antenna in 3 m dish at Barrett Range Experiment Ground WebSite and Results iGate page shows WLAN LQI iTag page shows association and RSSI Aluminum Hub, ribs, hinges, springs, on assembly mandrel Aluminum canister holds stowed antenna Before assembly into payload bay Internet Navigation Flight Controls iControl payload & mission com Aeneas mission control at ISI Hurricane mission hub, data storage Aeneas web server Rigel backup mission Hub Novawurks Inc. Barrett range USC Ham Shack SRI range Local LA antennas primarily for amateur band beacon collect Worldwide antennas amateur band beacon collect CA antennas Primarily for MHX primary radio Launch – Vandenberg AFB Integration Jan 2012 Launch NROL 36 Sept 13, 2012 P-POD Integration at Cal Poly Deployment Testing Full Launch and Early Ops test antenna downward Subsequent test antenna upward Integrated and Stowed at USC/ISI Mission Operations Overview Amateur Radio QSL card back ~640g Maximum at Feed Stowage Fixture Mysql search of 28652 shows handful of Non-Zero LQI At least two of were observed during AOS Indicates RF activity consistent with WiFi MATTS Tag Operational

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Page 1: J.Tim Barrett, Dr. Mike Obal, Mike Aherne, Dr. Tatiana

L-36 Atlas V launch vehicle • Orbit

− Altitude 470km – 780km − Inclination 64 degrees

• Date − Delivery January 2012 − Flight September 2012

World’s largest deployable from a NanoSat and first attempt at ground point tracking

Accomplished to date

J.Tim Barrett, Dr. Mike Obal, Mike Aherne, Dr. Tatiana Kitchkaylo, Jeff Sachs, Lucy Hoag, Will Bezouska, Craig Ward, Emin Vartanians, Alexader Shim, Siamak Hesar, Eric Teegarden, Rohan Ramadas, Melissa Christensen, Michael Ortega, Melissa Jawaharlal, Omair Rahman, Amit Shah, Anthony Shao, Nate White, John Razzano, Sara Gramling, Rahul Karkhanis, Chunyih Hsu, Dayung Koh, Neha Rathore, Carson Vogt, Erin Fowler, Amparo Romero, Desiree Webster, Xiaodan Wu, Maria Guzman, Amit Shah, Pezhman Zarifian, Andrew Laskowski, Mike Zarem, Michael Martin, Joe Parsons, Sammi Westall, Rafael Nuguid, Josh Fogel and Anubhav Thakur.

Aeneas Got Aperture?

Aeneas Got Aperture?

The Aeneas Mission

• Space based tag tracking experiment

− Space implementation of Marine Asset Tag Tracking System

(MATTS) by iControl Inc. − Bi-directional 2.4GHz comm. link

for Wireless Sensor Network − Ultra sensitive receiver to

communicate with low power, small, earth based sensors

− System currently uses ground stations ~ 1 mile range from ports

• Proof-of-concept: Satellite-based receivers for open ocean or cross

country • iControl data format selected for DHS

“Secure Corridors” Program

Various Publications: AIAA Space - Caerus Concept to Flight 11 months, SERC Engineering Teaching Hospital, Aeneas Three-Axis Pointing , Doppler-Based TLE Prediction and Correction and Current USU Small Sat Submissions

The authors wish to thank: David Barnhart for mission conception and guidance, the Cubesat Program Office for Colony I and access to launch, Prof. Joe Kunc and Maurice Martin at ORS/AFRL, Congresswoman Jane Harman’s office and ISI Executive Office for funding support.

Mission Enabler ½ meter deployable parabola

Bus: Colony I -USC Enhanced Three axis stabilized for sun and

ground tracking ±1.5° pointing accuracy Mems Gyros Sunsensor

Deployable Arrays with 22 watts full sun

Primary radio 115/248kbps 437.0 MHz spread

spectrum radio Secondary radio

1200 baud AFSK AX.25 Beacon @ 437.6 MHz Amateur Band

Dual Processor (FSW - C&HD) Payload: 0.5 m Deployable

parabolic antenna 18 dbi at 2.4GHz Space based implementation of

Marine Asset Tag Tracking System (MATTS)

Bi-directional 2.4GHz communication link for Wireless Sensor Network

Ultra sensitive receiver to communicate with low power, small, earth based sensors

The Colony I Bus Becomes Aeneas

World’s first – ½ Meter Deployable Antenna from CubeSat Filed invention disclosures for the device & processes with USC Stevens Institute

USC/ISI plans to provide advanced antenna to others

Stowed Antenna Link and Plug

LinkVespel- .25” dia x 3.5” long

#5 heli-coil

Rub plugMaterial TBD

Requirements Concepts/Prototype

Design/Implementation

Deployment Shock – Wyle Labs Anechoic RF – USC UltraLab

Closing the Link Required 18 dB gain on SV

Mobile Asset Tracking Tag

Frame from Stereolith Model Deployment Video

Solidworks Rendering

Metrology Testing - JPL

-90

-80

-70

-60

-50

-40 180

195 200 205 210 215 220 225 230 235

240 245 250 255 260 265 270 275 280 285 290 295

300 305

310 315

320 325

330 335 340 345 350 355 360 5 10 15 20 25 30 35 40

45 50

55 60

65 70 75 80 85 90 95 100 105 110 115

120 125

130 135 140 145 150 155 160 175

step 0 z=0 deg

step 0 z=0 deg -90

-80

-70

-60

-50

-40 180

195 200 205 210 215 220 225 230

235 240

245 250 255 260 265 270 275 280 285 290 295

300 305

310 315

320 325

330 335 340 345 350 355 360 5 10 15 20 25 30 35 40

45 50

55 60

65 70 75 80 85 90 95 100 105 110 115

120 125

130 135 140 145 150 155 160 175

Helix Alone

Helix Alone

Helix alone -55 dBm (l.) with Parabola -40 dBm (r.) yields 15 dBm gain

JPL collaboration Mark Thomson Spacecraft Antennas

March 2013

Antenna Stowage

10x10x16.5 cm Payload Bay

Hand wound Bifilar Tx & RX Helix(es) and test board

Field RF Testing

Los Angeles Basin -20 Miles Malibu to Playa Del Rey ground station

iGate Receiver and sector antenna in 3 m dish at Barrett Range

Experiment Ground WebSite and Results

iGate page shows WLAN LQI iTag page shows association and RSSI

Aluminum Hub, ribs, hinges, springs, on assembly mandrel Aluminum canister holds stowed antenna

Before assembly into payload bay

Internet

Navigation Flight Controls iControl payload & mission com

Aeneas mission control at ISI

Hurricane mission hub, data storage Aeneas web

server

Rigel backup mission Hub

Novawurks Inc. Barrett range USC Ham Shack

SRI range

Local LA antennas primarily for amateur band beacon collect

Worldwide antennas amateur band beacon collect

CA antennas Primarily for MHX primary radio

Launch – Vandenberg AFB

Integration Jan 2012 Launch

NROL 36 Sept 13, 2012

P-POD Integration at Cal Poly

Deployment Testing

Full Launch and Early Ops test

antenna downward Subsequent test antenna upward

Integrated and Stowed at USC/ISI

Mission Operations Overview

Amateur Radio QSL card back

~640g Maximum at Feed

Stowage Fixture

Mysql search of 28652 shows handful of Non-Zero LQI At least two of were observed during AOS Indicates RF activity consistent with WiFi MATTS Tag Operational