THE CANOP CUBESAT MISSION - REMOTE IMAGING OF THE RAIN FOREST AND TESTING AI BASED IDENTIFICATION TOOLS SSC20-V-06 SMALL SATELLITE CONFERENCE ...

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THE CANOP CUBESAT MISSION - REMOTE IMAGING OF THE RAIN FOREST AND TESTING AI BASED IDENTIFICATION TOOLS SSC20-V-06 SMALL SATELLITE CONFERENCE ...
The
CaNOP Cubesat Mission
Remote Imaging of the Rain Forest And Testing AI
Based Identification Tools
SSC20-V-06
Small Satellite Conference

  Andrew Santangelo              Dr. Kevin Crosby
    sci_Zone, Inc.               Carthage College
THE CANOP CUBESAT MISSION - REMOTE IMAGING OF THE RAIN FOREST AND TESTING AI BASED IDENTIFICATION TOOLS SSC20-V-06 SMALL SATELLITE CONFERENCE ...
Canopy Near-IR Observing Project

•   CaNOP Mission Overview
•   CaNOP CubeSat
•   Camera System
•   Mission Operations
•   LinkStar System

                                    sci_Zone, Inc.
                                   www.sci-zone.com
THE CANOP CUBESAT MISSION - REMOTE IMAGING OF THE RAIN FOREST AND TESTING AI BASED IDENTIFICATION TOOLS SSC20-V-06 SMALL SATELLITE CONFERENCE ...
CaNOP Mission Overview
Purpose:
•   Test method for Multispectral
    Imaging
•   Image changes in the rain forest
    on Earth
•   Visualize Changes in urban night
    lighting due to the growth of low
    power LED street lights
•   Identification of objects
    approximately the size of a 737
    in flight
                                         sci_Zone, Inc.
                                        www.sci-zone.com
THE CANOP CUBESAT MISSION - REMOTE IMAGING OF THE RAIN FOREST AND TESTING AI BASED IDENTIFICATION TOOLS SSC20-V-06 SMALL SATELLITE CONFERENCE ...
CaNOP Cubesat

                  sci_Zone, Inc.
                www.quick-sat.com
THE CANOP CUBESAT MISSION - REMOTE IMAGING OF THE RAIN FOREST AND TESTING AI BASED IDENTIFICATION TOOLS SSC20-V-06 SMALL SATELLITE CONFERENCE ...
Ver. 1.1 July 5, 2016
                                                                                                                Fig. 4.
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                                                                                           Hheight          is assumed to be the orbital altitude H = 400 km.                                      +)
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                                                                                                 Ver. 1.1 July 5, 2016
     Figure 3: msCAM multispectral camera with lens                        i                                        height is assumed
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                                                                                                                                                                    19
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                               Figure                                                                                                          &                                      19
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    2Field of View: The FOV(o) is a function of the sensor                                                                                                                                                      hy =11.86 mm (11.86/8 Fig. 4. Push
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     direction is therefore        The image properties obtained from a push broom sensor
                       time it takes the sensor to move a distance of 250 x GSD = 15.75 km. The along-track FOV                       19                                                                                                                                1FNW]   − PMQ
                                   moving along a scan track    Fig. 4.are  characterized        Dwell Time:
                                                                             Figure 4: Pushbybroom
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                                                                                                                                                                              pixel coverage
                                                                                                                                                                                      and is related directly to the signal-to-nois                  Swath Width: The    swath
                                                                                                                                                                                                                                                                     hy =11.86
                                                                                                                                                                                                                                                                     Swath       width
                                                                                                                                                                                                                                                                                mm
                                                                                                                                                                                                                                                                              Width: (1
                                   imaging is illustrated incharacterized
                                                              Figure 5. by the following quantities. The geometry of pushbroom imaging is illustrated
                              is 126 km (for a GSD         in Fig. 5. of 63 m). The cross-track image width is L = 67 km for an area of 9112                                                                                     Swath
                                                                                                                                                                                                                                scale   on theWig                    direction
                                                                                                                                                                                                                                                     the width of each strip ofisimag
                                                                                                                                                                                                                                                                                  there

                                  2Field of View: The FOV(      o
                                                                  ) View:
                                                                    is a Thefunction     ofa function
                                                                                              the sensor                                                                     pushbroom    sensor,  the dwell  time   is
                                                                                                                                                                                                                 height isrelated
                                                                                                                                                                                                                           assumed
                                                                                                                                                                                                                                of
                                                                                                                                                                                                                                 the
                                                                                                                                                                                                                                     to to
                                                                                                                                                                                                                                        be
                                                                                                                                                                                                                                    image    the
                                                                                                                                                                                                                                           the
                                                                                                                                                                                                                                        width
                                                                                                                                                                                                                                                o
                                                                                                                                                                                                                                             data
                                    . Let usand
                              km dimensions       assume   Field of8 lens.
                                                                        exposures
                                                                                FOV(º)  is        across
                                                                                                      of the      the 2 Mpx sensor in the 16.4 seconds required for
                                                                                                              sensor dimensions  and  the focal length of the
                                                                                                                                                                                                                                The imaging
                                                     the focal   length
                                                           objective         of sensor
                                                                             Our the objective        lens.
                                                                                         has dimensions    of h = 5.93 mm in the cross-track direction and
                                                                                                                 x                                                           km, the orbital velocity V= 7.67 km/sec.
                                                                                                                                                                                                                 0 = 2bPQW TU9/2
                                                                                                                                                                                                                                Hheight
                                                                                                                                                                                                                                        = 67is Sca
                              each band to passdirection
                                   Our  sensor has dimensions  along
                                                                 of
                                                           h =11.86
                                                                 y    h mm
                                                                         x =   126 km of the track. At 10 bits/pixel, the data acquired along the
                                                                              5.93
                                                                            (11.86/8
                                                                      is therefore
                                                                                    mm
                                                                                     = 1.48inmmthe  cross-
                                                                                                  per band) in the along-track direction. The FOV in each                                                                           = 400 km
                                   track direction and hy =11.86 mm (11.86/8 = 1.48 mm                                                     6                     8                                               Ground Sample Swath     Width:The
                                                                                                                                                                                                                                  Distance:     Th
                              imaging
                                   per band)track     is (8 exposures)
                                              in the along-track    direction. CMNOO
                                                                                   The −FOVxPMQRS(10bits/px)
                                                                                                  in  each               x   (2x10           px)     =    1.6x10   bits = 20 MB.                                                 the width of eac
                                                                                                                                                                                                                                 0 = 2bPQ
                                    direction is therefore
                                                                                                  TU9 V = 2PQW
                                                                                1FNW] − PMQRS TU9 V^ = 2PQW
                                                                                                             )
                                                                                                                     +)
                                                                                                                          +)
                                                                                                                        ℎ /2L = 9.68º
                                                                                                         Fig. 4. ℎPushbroom
                                                                                                                   _ /2L = 2.43º/aQWB
                                                                                                                                          Y

                                                                                                                              sensor showing the arrangement of 2 Mpx into 8 spectral bands.
                                                                                                                                                                                                                                        Pi = @>=/9  = 63 c/(7.67×
                                                                                                                                                                                                                                                             height is assume
                                                                                                                                                                                                                                                 @>= = B ×b/L = (5.5e10             +f
                                                                                                                                                                                                                                                               &
                                                                                                                         Figure 4: Push broom sensor showing the
                                                                                                                                                                                                                                                                  0 = 2bPQW TU9
                                                                                                                                                                                                                                                                  Ground
                                                               Swath Width: The swath width L is the cross-track
                                                                                                       The image image arrangement
                                                                                                                       scale on
                                                                                                                   properties             ofIt a2represents
                                                                                                                                the ground.
                                                                                                                              obtained  from        Mpx intosensor
                                                                                                                                                   pushbroom  8 spectral  bands.
                                                                                                                                                                   moving along a scan track are
                                                                                                                                                                                                                                                                   GroundSam  S
                                                               the width of each strip of image data acquired   in a pass over
                                                                                                          characterized
                                                               height is assumed to be the orbital altitude
                                                                                                          in H = 400
                                                                                                             Fig. 5. km.
                                                                                                                               thefollowing
                                                                                                                          by the    target terrain. The imaging
                                                                                                                                              quantities.
                                                                                                                                                                                              A dwell time of 8.2 msec suggests a
                                                                                                                                                          The geometry of pushbroom imaging is illustrated
                                                                                                                                                                                                                                                              shutter  time
                                                                                                                                                                                                                                                                  projected
                                                                                                                                                                                                                                                                  Ground    pix
                                                                                                                                                                                                                                                                         Sample

                                                               0 = 2bPQW TU9/2 = 67 Sc.                                                                                                       of ofthe
                                                                                                             Field of View: The FOV(º) is a function of the sensor dimensions and the focal length  the camera unit under consideration for the
                                                                                                                                                                                                                                          @>=
                                                                                                                                                                                                                                          @>= = B Ca
                                                                                                                                                                                                                                                 =×b/L
                                                                                                                                                                                                                                                    B&                         &

                                                                                                    objective
                                                               Ground Sample Distance: The GSD is the           lens. Ourpixel
                                                                                                      ground projected    sensor
                                                                                                                               size:has dimensions of hx = 5.93 mm in the cross-track direction and
                                                                                                    hy =11.86 mm (11.86/8 = 1.48 mm per band) in the along-track direction. The FOV in each
                                                               @>= = B& ×b/L = (5.5e10+f c)×(400×10 direction
                                                                                                       (       is therefore
                                                                                                                      +(
                                                                                                         c) / (35×10     c) = 63 c.
                                                                                                                                                                        To estimate           the image size          in bytes of a strip of im
                                                                                                                                                    CMNOO − PMQRS TU9 V) = 2PQW+)
                                                                                                                                                                                 Figure 3: msCAM multispectral
                                                                                                                                                                                               ℎY /2L = 9.68º
                                                                                                                                                                                                                sci_Zone,
                                                                                                                                                                                                                  camera with lensInc.
                                                                                                                                                                        derived here,           weintoconsider
                                                                                                                                                                                        integrated      the cubesat a  frame rate of 1 expos
                                                                                                                                                                                                                    structure
                                                                                                       1FNW] − PMQRS TU9 V = 2PQW          ℎ /2L = 2.43º/aQWB      ^
                                                                                                                                                                          19
                                                                                                                                                                            +)
                                                                                                                                                                                           _
                                                                                                                                                                                                           www.sci-zone.com
                                                                                                                                                                               The image properties obtained from a push broom sensor
                                              Figure 5: Push broom imaging geometry. Swath Width: The swath width L is the cross-track image scale on the ground. It time
                                                                                                                                                                        representsit takes the sensor to move a distance of 250
                                                                                                                                                                               moving along a scan track are characterized by the
                                              Fig. 5. Pushbroom imaging geometry.    the width of each strip of image data acquired in a pass over the target terrain. The imaging
                                                                                     height is assumed to be the orbital altitude H = 400 km.                           is   19.2º,
                                                                                                                                                                               followingwhich      provides
                                                                                                                                                                                           quantities.          a total
                                                                                                                                                                                                       The geometry        exposure
                                                                                                                                                                                                                      of push  broom  track of
THE CANOP CUBESAT MISSION - REMOTE IMAGING OF THE RAIN FOREST AND TESTING AI BASED IDENTIFICATION TOOLS SSC20-V-06 SMALL SATELLITE CONFERENCE ...
Mission Operations
The primary mission of CaNOP is to return spectrally resolved images
of diverse forest landscapes from a variety of ecological and
climatological niches.

•     Launch to ISS by NASA/ELaNA
•     Deployed from Nanoracks
      Cubesat launch container
•     De-tumbling begins 30 minutes
      after deployment for one orbit
•     Imaging activated when
      crossing defined “fences”

Imaging Targets:
•   Los Katíos National Park is located in Colombia, South America
•   El Caura in Venezuela, South America
•   Sangha Tri-National Forest is an equatorial tropical rainforest situated between the
    nations of Central African Republic, Cameroon and Congo-Brazzaville                     sci_Zone, Inc.
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THE CANOP CUBESAT MISSION - REMOTE IMAGING OF THE RAIN FOREST AND TESTING AI BASED IDENTIFICATION TOOLS SSC20-V-06 SMALL SATELLITE CONFERENCE ...
LinkStar Architecture
LinkStar: A Paradigm Shift
THE CANOP CUBESAT MISSION - REMOTE IMAGING OF THE RAIN FOREST AND TESTING AI BASED IDENTIFICATION TOOLS SSC20-V-06 SMALL SATELLITE CONFERENCE ...
sci_Zone, Inc.                                                                               AF192-001                   F192-001-1674

                                  LinkStar-TRK,-STX3

 GSP-1720
 Satellite Data and Voice Module

GSP-1720
                                                     LinkStar-D
                               The GSP-1720 Satellite Data and Voice Module (SDVM)
                               provides full, two-way data and voice capability, allowing for

Satellite Data and Voice Modulethe development of new and creative applications from basic
                               AT Modems to fully-featured fixed telephone services from
                               remote locations.

                                                                                                                                           OEM-719, ADA Fruit
 Features and Advantages:                             The GSP-1720 Satellite Data and Voice Module (SDVM)
                                            SCADA Applications:
                                                                                                                                             UltimateGPS
                                                      provides full, two-way data and voice capability, allowing for

                                                                                                                                                GPS
                                                      the development of new and creative applications from basic
                                                      AT Modems to fully-featured fixed telephone services from

                                             LinkStar-HD                                                                QuickSat
                                            GSP-1720 Includes:
                                                      remote locations.
 Data Services:

                                            Installation Options

Features and Advantages:                                                     SCADA Applications:

                                            Other radios                     GSP-1720 Includes:
                                                                                                                            Industrial
                                                                                                                        BeagleBone Black
                                                                                                                           Flight
Data Services:

                                                                                                                                             MAI-400
                                                                             Installation Options

                                                                                                                         Computer

                                                                                                                                             Sensors
                       LinkStar
                       Architecture                                                                                                         Actuators
                                                                                                                                               sci_Zone, Inc.
                                                                                                                       Other Computers        www.sci-zone.com
                                                                                                                                                                     8
THE CANOP CUBESAT MISSION - REMOTE IMAGING OF THE RAIN FOREST AND TESTING AI BASED IDENTIFICATION TOOLS SSC20-V-06 SMALL SATELLITE CONFERENCE ...
LinkStar-STX3-PC104
Globalstar STX3 Based Module
 • Power
     •   192 mW Tx power
 •   PC104 Based
 •   Full Support for Cubesat Bus
 •   Beagle Bone Black Cape Interface
 •   Duplex Radio, any radio interface
 •   Supports switched/unswitched power
 •   Serial, I2C interface
 •   GPS Interface (NovAtel, Adafruit)
 •   Near Global Coverage!

 sci_Zone, Inc.
www.sci-zone.com
THE CANOP CUBESAT MISSION - REMOTE IMAGING OF THE RAIN FOREST AND TESTING AI BASED IDENTIFICATION TOOLS SSC20-V-06 SMALL SATELLITE CONFERENCE ...
sci_Zone, Inc.
www.sci-zone.com
Satellite Data and Voice

 LinkStar Duplex
 Product Features                                                                     Th
                                                                                      pro
                                                                                      the

• No deployables                                                                      AT
                                                                                      rem
• 3 cm diameter circular patch for duplex
• Rapid acquisition
• Data rates
•   9600 bps maximum
•   SMS Uplink Messaging
•   LinkStar intended to compliment traditional high speed
                                                  Features and radios
                                                               Advantages:

•   LinkStar can serve as a primary radio depending project and
    product data requirements.

                                                                    sci_Zone, Inc.
                                                                   www.sci-zone.com
LinkStar Product Features
 •   Almost anytime, anywhere vehicle Telemetry, Tracking and Control

 •   Large, global coverage area

 •   Common FCC Satellite-to-Satellite License

 •   No Amateur bands

 •   No satellite to ground license required

 •   Globalstar will work with sci_Zone on obtaining FAA and FCC licenses

 •   Ground station over Internet Protocol (IP)
 •   Access your vehicle from anywhere!
 •   Piggy-backs on established 2 billion dollar network
 •   Low Cost

                                                              sci_Zone, Inc.
                                                             www.sci-zone.com
sci_Zone, Inc.
www.sci-zone.com
GPS Interface
•   NovAtel OEM 719
    •   COCOM limits removed
    •   Acquisition time in space 4 - 6 minutes (one time took
        18 minutes).
    •   Lock maintained for multiple orbits
    •   Can look below the horizon
    •   Antenna placement critical

•   Adafruit Ultimate GPS
    •   Can work above 59,000 feet

                          LinkStar radios
                         auto sense GPS

                           APIs provided
Interface   Message and GPS
               information

                                    Radio
                                 messaging
                                 control and
                              radio information

                                GPS signal
                                   quality
                                information

                              OEM 719 Accepts
                                SNR > 29 db
• Web server - html 5/
   javascript, php
                                                    QuickSAT/
                                                      VMS                Architecture
   •C
   • Python                                                 Custom Interfaces

         Custom & Addon
           Processes
                                               stepSATdb_Flight

                                                     vms_db

        Custom Commands                               vms
                                                       Core Commands

                                               Communication Tools
APIs created for                                     lsRadio
communication system
interface, database interface
and communicating with the
GPS (Adafruit and NovAtel).                       Command
                                Applications                      Data
                                                    Files

                                                                                 sci_Zone, Inc.Inc.
                                                                                     sci_Zone,
                                                                                www.sci-zone.com
                                                                                  www.sci-zone.com
QuickSAT/Autonomy
 with LinkStar
QuickSAT/Autonomy can be used to fuse sensor data,
such as data from hyperspectral cameras and other
sensors to sense and perceive events and conditions. The
event/condition is transmitted to the ground - the cubesat
can autonomously act on the event/condition. The event/
condition can be transmitted efficiently and quickly (in as
little as 0.2 seconds depending on the radio system). The
operator can download the large raw data as needed at a
later time.

   Autonomy APIs and Functions for Vehicle Health Monitoring,
   Perception and Planning

   Integrated computer (BeagleBone AI or Xilinx Zynq UltraScale+
   MPSoC chip), communications interface, with optional GPS.

   IC2, Space Wire, Serial, CAN, USB interfaces, UART

   Support for CubeSat bus

   0.5 U in size

   QuickSAT/VMS environment for seamless control and software
   integration

   Optional Hypervisor for protection from malicious attacks.
                                                                    sci_Zone, Inc.
                                                                   www.sci-zone.com
                                                                                  17
Next STEP - Join the Fun!
  email: andrew_santangelo@sci-zone.com
  web: www.sci-zone.com

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