Computing

Very precise colour data is recorded with the GreenEye Visible NIR hyperspectral imaging camera. In contrast to colour cameras, it reproduces spectral information in more than 1000 bands. It combines the visible and NIR spectrums, allowing conclusions to be drawn regarding chemical characteristics, including material properties.

Here are some of its main attributes:

RedEye – NIR Hyperspectral Camera from INNO-Spec is a line of push-broom HSI cameras for the near-infrared (NIR) spectrum that can operate in wavelengths between 950 and 2200 nm. It is available in four versions with varying wavelength ranges and offers real-time in-line monitoring, even on fast-moving objects.

RedEye NIR HS Cameras offer various wavelength ranges, excellent photosensitivity, GigE Vision Interface, parallel colour image recording, best optical image quality, and are maintenance-free.

• Industry-standard camera adapter socket for use with a wide range of CSI, GMSL, and other cameras
• 10Gb Ethernet + 1GB Ethernet ports
• Wide temperature operation – matching the range of the Orin module
• Dual minicard sockets with PCIe and USB interfaces
• Dual M.2 sockets for flash memory (M key 2242/2280) and network connectivity (E key 2230)
• I/O concentrator connector enables use with standard and custom I/O breakout boards

• Supports all I/O features of Jetson Nano / Xavier NX / TX2 NX modules
• Compact size 4.3×3.3″ / 110x85mm
• Single/dual gigabit Ethernet
• 1x USB 3.1, 2x USB 2.0
• HDMI + DisplayPort
• 3x CSI dual lane camera inputs
• 2x serial ports: 1 RS-232 and 1 RS-232/485
• 16 GPIO with 3.3V / 5V compatibility
• 1 CAN port (with NX module)
• M.2 2242/2280 M-Key NVMe flash socket
• Heat sink / fan sink cooling (orderable options)
• Expansion connector for use with standard and custom I/O expansion modules
• 7-24VDC power input
• Supports full temperature range of installed Jetson modules, -25 to +80ºC
• Available as carrier board, subassembly with installed Jetson module and software, or complete system

• 2 x Redundant MIL-STD-1553 Channels
• 8 x ARINC-429/575 Tx/Rx Channels
• 8 x RS-232/422/485 Sync/Async Serial Channels
• 28 VDC Input PSU with 50 ms holdup option

• 2 x Redundant MIL-STD-1553 Channels
• 8 x ARINC-429/575 Tx/Rx Channels
• 8 x RS-232/422/485 Sync/Async Serial Channels
• 28 VDC Input PSU with 50 ms holdup option

with 10 GB Fiber Optic & 1 GB Copper Ethernet Switch

• Preconfigured embedded I/O Functions: 24-CH Discrete I/O, 8-CH ARINC 429/575, 4-CH CANBus (programmable for CAN 2.0A/B, ARINC 825 or CAN FD protocol) and 2-CH MIL-STD-1553
• Ethernet switch module that offers four (4) 10GBase-SR multimode fiber optic ports and sixteen (16) 10/100/1000Base-T Ethernet ports
• Supports One NAI smart I/O function module
• Minimized SWaP Footprint
• Xilinx UltraScale+ SoC with Dual/Quad Core ARM Cortex®-A53 processors
• 28 VDC Input Power Supply (50+ ms Hold-up Option)
• DO-178C & DO-254 DAL A (Contact Factory)
• Cybersecurity & Anti-Tamper (Contact Factory)

6x 3U OpenVPX MOSA Remote Interface Unit

• 2 x MIL-STD-1553 & 8 x ARINC-429 Tx/Rx (CM5)
• 8 x RS-232/422/485 Serial Channels (SC3)
• 8 x CANBus A/B 2.0/CAN-FD/ARINC-825 (CB8)
• 8 x Programmable RTD or Thermocouple measurement (TR1)
• 16 x ±100 VDC A/D Channels (ADF)
• 8 x ±40 VDC 100 mA Digital to Analog Channels (DA3)
• 2 x AC Reference Excitation (AC2)
• 4 x Strain Gage Measurement (SG1)
• 8 x Variable Reluctance/Pulse Counter Measurement Channels (VR1)
• 16 x 10/100/100 Base-T Ethernet Switch (ES2)
• 48 x Discrete Input Channels and 48 Programmable Discrete I/O Channels (68DT1)
• 28 VDC MIL-STD-704 Aircraft Electrical Power Characteristics with at least 50 ms holdup.
• MIL-STD-810G, MIL-STD-461F and DO-160 environmental and EMI/EMC qualifications.

4x 3U OpenVPX MOSA Remote Interface Unit

• 2 x MIL-STD-1553 & 8 x ARINC-429 Tx/Rx (CM5)
• 8 x RS-232/422/485 Serial Channels (SC3)
• 8 x CANBus A/B 2.0/CAN-FD/ARINC-825 (CB8)
• 8 x Programmable RTD or Thermocouple measurement (TR1)
• 8 x ±40 VDC 100 mA Digital to Analog Channels (DA3)
• 2 x AC Reference Excitation (AC2)
• 4 x Strain Gage Measurement (SG1)
• 8 x Variable Reluctance/Pulse Counter Measurement Channels (VR1)
• 48 x Discrete Input Channels and 48 Programmable Discrete I/O Channels (68DT1)
• 28 VDC MIL-STD-704 Aircraft Electrical Power Characteristics with at least 50 ms holdup.
• MIL-STD-810G, MIL-STD-461F and DO-160 environmental and EMI/EMC qualifications.

6x 3U OpenVPX MOSA Mission Computer

• 2 x MIL-STD-1553 & 8 x ARINC-429 Tx/Rx (CM5)
• 8 x RS-232/422/485 Serial Channels (SC3)
• 8 x CANBus A/B 2.0/CAN-FD/ARINC-825 (CB8)
• 4 x MIL-STD-1553/1760 (2 x FTJ)
• 4 x Non-Latching Relay (RY1)
• 24 x Enhanced Programmable Discrete I/O Channels (DT4)
• 16 x ±100 VDC A/D Channels (ADF)
• 12 x ±10 VDC or ±25 mA D/A Outputs (DA1)
• 12 x ±1.25 to ±10.0 A/D Channels (AD1)
• 12 x ±100V A/D Channels (AD2)
• 16 x ±1.25 to ±10.0 VDC A/D Channels (AD4)
• 16 x 10/100/100 Base-T Ethernet Switch (ES2)
• 48 x Discrete Input Channels and 48 Programmable Discrete I/O Channels (68DT1)
• 28 VDC Input PSU per VITA 62 (VPX68) Optional 50 ms holdup.
• MIL-STD-810G, MIL-STD-461F and DO-160 environmental and EMI/EMC qualifications.

4x 3U OpenVPX MOSA Mission Computer

• 2 x MIL-STD-1553 & 8 x ARINC-429 Tx/Rx (CM5)
• 8 x RS-232/422/485 Serial Channels (SC3)
• 8 x CANBus A/B 2.0/CAN-FD/ARINC-825 (CB8)
• 24 x Enhanced Programmable Discrete I/O Channels (DT4)
• 16 x ±100 VDC A/D Channels (ADF)
• 12 x ±10 VDC or ±25 mA D/A Outputs (DA1)
• 16 x 10/100/100 Base-T Ethernet Switch (ES2)
• 48 x Discrete Input Channels and 48 Programmable Discrete I/O Channels (68DT1)
• 28 VDC Input PSU per VITA 62 (VPX68) with Optional 50 ms holdup.
• MIL-STD-810G, MIL-STD-461F and DO-160 environmental and EMI/EMC qualifications.

2x 3U OpenVPX MOSA Mission Computer

• 2 x MIL-STD-1553 & 8 x ARINC-429 Tx/Rx (CM5)
• 8 x RS-232/422/485 Serial Channels (SC3)
• 8 x CANBus A/B 2.0/CAN-FD/ARINC-825 (CB8)
• 24 x Enhanced Programmable Discrete I/O Channels (DT4)
• 16 x ±100 VDC A/D Channels (ADF)
• 12 x ±10 VDC or ±25 mA D/A Outputs (DA1)
• 28 VDC Input PSU per VITA 62 (VPX68). Optional 50 ms holdup.
• MIL-STD-810G, MIL-STD-461F and DO-160 environmental and EMI/EMC qualifications.

2x 3U OpenVPX MOSA Flight Control Computer

• 8 x ARINC-429 Tx/Rx & 12 Programmable Discrete IO (CM2)
• 16 x ±100 VDC A/D Channels (ADF)
• 8 x Programmable RS-232/422/485 Serial Channels (SC3)
• 2 x AC Excitation References (AC2)
• 4 x LVDT Measurement Channels (LD2)
• 4 x ±40 VDC 100 mA Digital to Analog Channels (DA3)
• 28 VDC Input PSU per VITA 62 (VPX68) with at least 50 ms holdup
• MIL-STD-810G, MIL-STD-461F and DO-160 environmental and EMI/EMC qualifications.

• I/O breakout from Xavier board:
• 2x USB 3.1
• 2x USB 2.0
• 2x Gigabit Ethernet
• 1x HDMI
• 1x LVDS LCD
• 4x RS-232/RS485/RS422
• 2x CAN 1Mbps
• Audio
• SAM DAQ circuit:
• 6 12-bit A/D, 0-3.3V input range, up to 1MSPS sampling rate
• 2 12-bit D/A, 0-3.3V output range
• 13 GPIO, 3.3V logic levels

• Complete system with Jetson AGX Xavier module and Linux OS installed m
• 2 gigabit Ethernet ports
• 2 HDMI 2.0a/b ports
• 2 USB 3.0 ports with type A connectors
• 2 USB 2.0 ports
• 4 serial ports with RS-232/422/485 (depending on model)
• Camera module connector supporting up to 12 lanes CSI
• 2 optional CAN ports
• 1 Mini PCIe socket with PCIe and USB support
• 1 M.2 2280 PCIe x1 socket
• Input voltage 9-20VDC; 12VDC universal AC adapter included
• Operating temperature -25 to +70°C
• Steel enclosure with aluminum heat sink
• Dimensions: 150 x 112 x 72mm / 5.9 x 4.4 x 2.8″

• I/O breakout from Xavier board:
• 2x USB 3.1
• 2x USB 2.0
• 2x Gigabit Ethernet
• 2x HDMI
• 4x RS-232/RS485/RS422
• 2x CAN
• Audio
• SAM DAQ circuit: 6xADC input to SAM controller and 2x DAC via SAM controller
• Digital IOs: 13 Digital IO via SAM controller