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UTC AEROSPACE SYSTEMS SU320CSX Operation Manual

Mil-rugged, high sensitivity, small swap ingaas swir camera
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SU320CSX
Operation Manual:
SU320CSX
Mil-Rugged, High Sensitivity, Small SWaP
InGaAs SWIR Camera
330 Carter Road
Suite 100
Princeton, NJ 08540 USA
Tel: (US) 609-333-8000
www.sensorsinc.com
4110-0446, Rev. B
Page 1 of 96
© 2016 UTC Aerospace Systems
Date Printed: 5-Dec-2016
This document does not contain any export controlled technical data.

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Summary of Contents for UTC AEROSPACE SYSTEMS SU320CSX

  • Page 1 InGaAs SWIR Camera 330 Carter Road Suite 100 Princeton, NJ 08540 USA Tel: (US) 609-333-8000 www.sensorsinc.com 4110-0446, Rev. B Page 1 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 2 4110-0446, Rev. B Page 2 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 3: Table Of Contents

    Pixel Clock Commands ..........................54     5.12. Frame and Exposure Control Commands ....................55 4110-0446, Rev. B Page 3 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 4 LIST OF ABBREVIATIONS ..........................  9 2     NOTES .................................  9 3   APPENDIX A: Camera Command Summary ....................  9 4 4110-0446, Rev. B Page 4 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 5: Introduction

    1. Introduction 1.1. Foreword This manual applies to all variants of the SU320CSX camera. These are collectively referred to as the CSX camera. Appendix B to this manual contains configuration information that is specific to your camera variant. It is included as a separate document on the mini-disc or media card that ships with the camera.

  • Page 6: System Contents

    Do not make or break the connection at the camera or on the cable while power is being supplied. See Section 2.1.3 for more information about the power interface. 1.3. System Contents A complete order for an enclosed SU320CSX may include the following:  SU320CSX camera body ...

  • Page 7: Safety Considerations

    See Table 1 for the case temperatures that correspond to each TEC setpoint. 4110-0446, Rev. B Page 7 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 8: Camera Cleaning

    It is important to use isopropyl alcohol because it acts as a lubricant when wiping the surface of the window. 4110-0446, Rev. B Page 8 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 9: Getting Started Guide

    Additional dimensions are provided in the mechanical drawings below (Figure 1 and Figure 2). 4110-0446, Rev. B Page 9 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 10 SU320CSX Figure 1. Mechanical drawing of enclosed CSX. 4110-0446, Rev. B Page 10 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 11 SU320CSX Figure 2. Mechanical drawing of OEM CSX. 4110-0446, Rev. B Page 11 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 12 SU320CSX Figure 3. Mechanical drawing of OEM CSX with optional ST4 board-to-board connector. 4110-0446, Rev. B Page 12 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 13 Do not make or break this connection while power is being supplied. 4110-0446, Rev. B Page 13 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 14 Digital ground through individual inductors. V- is tied to 4110-0446, Rev. B Page 14 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 15: Frame Grabber Options And Installation

    SUI may provide these outputs natively on the camera in the future. Contact SUI for more information. 4110-0446, Rev. B Page 15 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 16 Each frame grabber is designed to interface with specific hardware ports in 4110-0446, Rev. B Page 16 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 17 1. Shut down the laptop computer. 2. Insert the FrameLink Express Frame Grabber into the ExpressCard interface. 4110-0446, Rev. B Page 17 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 18: Sui Image Analysis Freeware

    Section 5.5 Configuration Commands. 4110-0446, Rev. B Page 18 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 19 These should be turned off for radiometric, machine-vision, and similar applications. ENH:ENABLE? Returns the state of in-camera Section 5.10.2 enhancements. 4110-0446, Rev. B Page 19 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 20: Camera Link Data Interface

    No connect Xclk+ No connect No connect Inner shield (camera GND) SerTC+ Inner shield (camera GND) 4110-0446, Rev. B Page 20 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 21 Reserved, Do not use Reserved, Do not use PWR_RTN PWR_IN PWR_RTN PWR_IN PWR_RTN PWR_IN PWR_RTN PWR_IN 4110-0446, Rev. B Page 21 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 22 Table 5. AUX/IO 14-pin connector (3M 12214-1150-00FR) signal assignment. SYNC-RTN SYNC-OUT TRIG-IN-RTN TRIG-IN RS232-RTN RS232-TX RS232-RX Figure 7. CSX Camera Link Timing Diagram. 4110-0446, Rev. B Page 22 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 23: Focal Plane Array Operation

    VGAIN voltages. The camera internally provides all bias voltages necessary for operation of the focal plane array. 4110-0446, Rev. B Page 23 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 24: Camera System Operation

    A basic signal flow diagram for the CSX camera system is shown. 4110-0446, Rev. B Page 24 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 25 See the command sections for more detailed information on the operation of the various camera functions supported by the CSX camera. 4110-0446, Rev. B Page 25 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 26: Camera Functions And Control Software Interface

    A carriage return <CR> ends each command. • All commands and arguments should be separated by white space. 4110-0446, Rev. B Page 26 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 27 Returned if configured for verbose response Command mode. ARGS]<CR> Response RESULT<CR> Command Always returned. Result > Command Always returned. Prompt 4110-0446, Rev. B Page 27 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 28: Startup Messaging

    Configuration can be altered and saved by the user to customize camera operation. The Factory 4110-0446, Rev. B Page 28 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 29 User Configuration non-volatile memory space using the CONFIG:SAVE and OPR:SAVE or OPR:UPDATE commands. 4110-0446, Rev. B Page 29 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 30 Appendix B document for table of OPR settings). Type unsigned integer 4110-0446, Rev. B Page 30 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 31 OPR. Setting Type Global Command OPR:START opr_number Parameters opr_number Return Values none 4110-0446, Rev. B Page 31 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 32 Range 0 to N Type unsigned integer Example OPR:SAVE -- command -- return value 4110-0446, Rev. B Page 32 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 33 5.5.11. Delete All Operational Configurations Description Deletes all operational configuration slots created by the user from 4110-0446, Rev. B Page 33 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 34: Serial Communication Interface Commands

    Setting Type Global Command BAUD:CURRENT baud_rate Parameters baud_rate Return Values none Range 57600 4110-0446, Rev. B Page 34 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 35 Setting Type Global Command BAUD:FUTURE baud_rate Parameters baud_rate Return Values none Range 57600 115200 230400 460800 4110-0446, Rev. B Page 35 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 36 Global Command ECHO:MODE mode Parameters mode Return Values none Range Echo off Echo received character 4110-0446, Rev. B Page 36 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 37 5.6.8. Get Echo Character Description Returns the echo character used for echo mode 2. Setting Type Global 4110-0446, Rev. B Page 37 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 38: Non-Uniformity Corrections (Nucs) Commands

    The correction commands allow the offset, gain, and pixel corrections 4110-0446, Rev. B Page 38 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 39 Sets the state of the offset correction. Offset correction compensates for dark current signal non-uniformity. Otherwise known as a Dark 4110-0446, Rev. B Page 39 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 40 The global offset can be disabled by setting its value to zero. Setting Type Global Command CORR:OFFSET:GLOBAL value Parameters value 4110-0446, Rev. B Page 40 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 41: Bad Pixel Corrections

    CORR:PIXEL state Parameters state Return Values none Range Enables Pixel Substitutions Disables Pixel Substitutions Type string 4110-0446, Rev. B Page 41 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 42 Removes flag to make pixel active Sets ON or OFF state to user-flagged pixels across all OPRs Type integer, string 4110-0446, Rev. B Page 42 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 43 5.8.6. Get Correction Bypass State Description Returns the state of the correction bypass. Setting Type Global 4110-0446, Rev. B Page 43 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 44 Returns the state of the pixel substitution map. Setting Type Global Command CORR:PIXEL:MAP? Parameters none Return Values state 4110-0446, Rev. B Page 44 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 45 <frames> <flash> <output> Return Values none Range Initiates an averaging of 32 frames of field offset 4110-0446, Rev. B Page 45 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 46 -- acquire cal offset data based on 64 frames and save in camera live (volatile) memory. 4110-0446, Rev. B Page 46 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 47: Automatic Gain Control (Agc) Commands

    Note: The image enhancement algorithm is not recommended for windowing operation or enhancement of uncorrected data. 4110-0446, Rev. B Page 47 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 48 Parameters state Return Values none Range Enables AGC Disables AGC Type string Example AGC:ENABLE ON 4110-0446, Rev. B Page 48 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 49 Returns the lowest operational setting available for use by the AGC algorithm. Setting Type Global Command AGC:OPR:LOW? Parameters none 4110-0446, Rev. B Page 49 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 50 0 to (number) limited by number of operational settings that currently exist. Type unsigned integer Example AGC:OPR:HIGH? -- query command 7 -- return value 4110-0446, Rev. B Page 50 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 51: Image Enhancement Commands

    5.10.1. Set Enhancement State Description Sets the state of the image enhancement algorithm. 4110-0446, Rev. B Page 51 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 52 Return Values none Range Enables Automatic Enhancements Disables Automatic Enhancements Type string Example ENH:AUTO ON 4110-0446, Rev. B Page 52 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 53 Range 0 to 5 Type unsigned integer Example ENH:AVG? -- query command 0 -- response 4110-0446, Rev. B Page 53 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 54: Pixel Clock Commands

    Returns the FPA pixel clock rate in Hertz. The CSX camera clock rate is 20750000 Hz (20.75MHz). Setting Type Global 4110-0446, Rev. B Page 54 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 55: Frame And Exposure Control Commands

    Command EXP value Parameters value Return Values none Range 1 to 16777214 Type unsigned integer 4110-0446, Rev. B Page 55 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 56 Return Values value Range 1 to 16777214 Type unsigned integer Example FRAME:PERIOD? -- query command 4110-0446, Rev. B Page 56 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 57: Trigger Commands

    A latency time delay of 5 - 6 clocks is possible due to the shape and impedance of the incoming trigger, and not added into the following discussion. 4110-0446, Rev. B Page 57 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 58 Section 5.12. The timing sequence of the camera for trigger mode 2 is shown in 4110-0446, Rev. B Page 58 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 59 The delay between this trigger transition and start of exposure is 5 to 6 pixel periods. The timing sequence of the camera for trigger mode 3 is shown in the Figure. 4110-0446, Rev. B Page 59 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 60 5.13.2. Get Trigger Mode Description Returns the trigger and timing mode. Setting Type Global Command TRIG:MODE? 4110-0446, Rev. B Page 60 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 61 5.13.4. Get Trigger Source Mode Description Returns the trigger source mode. Setting Type Global Command TRIG:SOURCE? Parameters none 4110-0446, Rev. B Page 61 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 62 TRIG:POL 0 5.13.6. Get Trigger Polarity Description Returns the trigger polarity. Setting Type Global Command TRIG:POL? 4110-0446, Rev. B Page 62 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 63 0 to 16777215 Type unsigned integer Example TRIG:DELAY? -- query command 1000 -- return value 4110-0446, Rev. B Page 63 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 64: Gain Commands

    Example GAIN:DIGITAL? -- query command (corresponding one of ) -- return value -- return value 4110-0446, Rev. B Page 64 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 65: Thermal Commands

    +/- 2 degrees Celsius. Setting Type Command FPA:TEMP? -or- FPA:TEMP? Kelvin Parameters none or Kelvin Return Values temperature 4110-0446, Rev. B Page 65 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 66 Range -20 to 80 Type integer Example TEC:SETPOINT? -- query command 22 -- return value 4110-0446, Rev. B Page 66 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 67 TEC lock signal is achieved. Queries while blocked are not received. Setting Type Global Command TEC:WAIT Parameters none 4110-0446, Rev. B Page 67 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 68: Digital Output Commands

    Range RAW Stage 1, Raw Data 12 bits Stage 2, Test Pattern 12 bit 4110-0446, Rev. B Page 68 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 69: Camera Information Commands

    9 character alpha numeric string Type string Example CAMERA:PN? -- query command 8000-0773 -- return value 4110-0446, Rev. B Page 69 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 70 9 character alpha numeric Type string Example FIRM:REV? -- query command 2.2 -- return value 4110-0446, Rev. B Page 70 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 71 9 character alpha numeric string Type string Example FPA:SN? -- query command 3713S5870 -- return value 4110-0446, Rev. B Page 71 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 72 136 yrs Type String Example ETM? -- query command Days:8 04:03:02 -- return value 4110-0446, Rev. B Page 72 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 73 Setting Type Command CMDS? [prefix] Parameters prefix (optional) Return Values value (command) Range Type string 4110-0446, Rev. B Page 73 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 74 “ON” argument. Error Description Cause Resolution 0 (LSB) PLL0 error Internal error Power cycle camera 4110-0446, Rev. B Page 74 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 75 Power Cycle Camera Alignment Error Correction Corr DL Download in No action required Suspend Progress 4110-0446, Rev. B Page 75 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 76 The command sets the flag; only a reboot will reset the flag to 0. Setting Type Command PWRDWN Parameters none 4110-0446, Rev. B Page 76 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 77 Example LED:ENABLE ON 5.17.21. Get LED State Description Returns the state of the status LED. 4110-0446, Rev. B Page 77 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 78: Binning Mode Commands

    5.18. Binning Mode Commands Binning Mode shifts SU320CSX camera imaging from a 320x256 to a 160x128 pixel mode of operation. Enabling Binning Mode produces a like sized image with each 2x2 bin equal to the average of the 4 individual pixels. To maintain compatibility with video and Camera Link signals, binned pixel results consist of the binned block’s pixels being set to the same value (value is repeated), and the full frame...

  • Page 79: Test Commands

    Enable test pattern TP2 ON TP3 Enable test pattern TP3 Disable test pattern Type string 4110-0446, Rev. B Page 79 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 80 FRAME:STAMP ON 5.19.4. Get Frame Stamp State Description Returns the Frame Stamp state. Setting Type Global 4110-0446, Rev. B Page 80 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 81: Macro Commands

    Final OK or ERROR with macro_ echo off , return values of any query commands contained in the macro with macro_ echo ON and 4110-0446, Rev. B Page 81 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 82: Windowing Commands

    Setting Type Operational Command WIN:COL:START value Parameters value Return Values none 4110-0446, Rev. B Page 82 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 83 Returns the stop column number for the ROI. Setting Type Operational Command WIN:COL:STOP? Parameters none Return Values value Range 3 to 316 4110-0446, Rev. B Page 83 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 84 Setting Type Operational Command WIN:ROW:STOP value Parameters value Return Values none 4110-0446, Rev. B Page 84 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 85 Gets the global corner row and column numbers for the ROI. Setting Type Global Command WIN:RECT? 4110-0446, Rev. B Page 85 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 86 0 to 255 for SU640HSX for corner column value Type unsigned integers Example WIN:RECT? X1:0 Y1:0 X2:217 Y2:111 -– return values 4110-0446, Rev. B Page 86 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 87: Specifications

    MIL-STD-461F, RE102 Mean Time Between Failure ≥ 10,000 hours per MIL-HDBK-217F with VITA51.1 supplement Fungus-Inert Material 4110-0446, Rev. B Page 87 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 88: Electro-Optic Performance Specifications

    The percentage of pixels with responsivity deviation less than 35% from the mean. 4110-0446, Rev. B Page 88 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 89: Product Support

    4110-0446, Rev. B Page 89 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 90: Customer Support

    Suite 100 Princeton, NJ. 08540, USA Tel: +1 609 333 8000 Fax: +1 609 333-8103 www.sensorsinc.com 4110-0446, Rev. B Page 90 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 91: Warranty

    4110-0446, Rev. B Page 91 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 92: List Of Abbreviations

    TTL: transistor-transistor logic (digital signaling standard) TEC: thermoelectric cooler UTAS: United Technologies Aerospace Systems UTC: United Technologies Corporation 4110-0446, Rev. B Page 92 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 93: Notes

    _____________________________________________________________________________________ _____________________________________________________________________________________ _____________________________________________________________________________________ _____________________________________________________________________________________ _____________________________________________________________________________________ _____________________________________________________________________________________ _____________________________________________________________________________________ _____________________________________________________________________________________ _____________________________________________________________________________________ _____________________________________________________________________________________ _____________________________________________________________________________________ _____________________________________________________________________________________ _____________________________________________________________________________________ _____________________________________________________________________________________ _____________________________________________________________________________________ 4110-0446, Rev. B Page 93 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

  • Page 94: Appendix A: Camera Command Summary

    ENH:AVG value ........53     5.10.6. Get Enhancement/AGC Frame Average Weight ENH:AVG? ..........53     4110-0446, Rev. B Page 94 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 95 BIN:ENABLE? ......... 79     5.19.1. Set Test Pattern State TESTPAT state ......... 79     4110-0446, Rev. B Page 95 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.
  • Page 96 WIN:RECT <X1> <X2> <Y1> <Y2> ..85     5.21.10. Get Window Rectangle WIN:RECT? ..........85     4110-0446, Rev. B Page 96 of 96 © 2016 UTC Aerospace Systems Date Printed: 5-Dec-2016 This document does not contain any export controlled technical data.

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