SAE AS 6129-2012 AS6129 Interface Standard Airborne EO IR Systems Electrical《AS 6129 电气机载光电 红外系统接口标准》.pdf

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4、0 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org SAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/AS6129 AEROSPACE STANDARD AS6129 Issued 2012-12 AS6129: Interface Standard, Airbo

5、rne EO/IR Systems, Electrical RATIONALE This document was created to standardize the data interface between aircraft and EO/IR sensors. This activity was initiated at the request of the U.S. Navy in 2009. PREFACE AS6129, Interface Standard, Airborne EO/IR Systems, Electrical, is a standard that defi

6、nes the electrical interface between aircraft (manned and unmanned) and onboard EO/IR Systems. Its purpose is to promote platform to sensor system interface standardization by providing substantial, but not 100% commonality, interoperability, and interchangeability. This document was prepared by the

7、 AS-1C1 Electro-Optic/Infrared Signal Sets Task Group, under the jurisdiction of the AS-1C Subcommittee, Avionic Subsystems, of the SAE AS-1 Committee, Platform Systems and System Integration. TABLE OF CONTENTS 1. SCOPE 3 1.1 Relationship Between Platform/Sensor Interfaces and SAE AS-1C Standards .

8、3 1.2 Purpose . 3 1.3 Application . 4 2. REFERENCES 4 2.1 Applicable Documents 4 2.1.1 SAE Publications . 4 2.1.2 Government Documents . 4 2.1.3 Industry Documents 5 2.2 Order of Precedence . 5 2.3 Definitions . 6 2.4 Acronyms 7 3. GENERAL REQUIREMENTS: INTERFACE CONFIGURATIONS 9 3.1 Platform/Sensor

9、 Configurations 9 3.2 Classes . 10 4. DETAILED REQUIREMENTS 10 4.1 Connector Characteristics . 10 4.1.1 Turret Class I - II Interface Connectors . 12 4.1.2 Turret Class III, Interface Connectors . 25 4.1.3 Turret Class IV Interface Connectors . 34 5. NOTES 42 SAE AS6129 Page 2 of 51 APPENDIX A ADDIT

10、IONAL INTERFACE REQUIREMENTS FOR GPS RF SIGNALS . 43 APPENDIX B RATIONALE DOCUMENTATION . 47 FIGURE 1 RELATED SAE STANDARDS 3 FIGURE 2 CONCEPTUAL PLATFORM/SENSOR INTERFACE CONFIGURATIONS . 9 FIGURE 3 LOCATIONS OF INTERFACES ASSUMING A HAND-CONTROLLER 10 FIGURE 4 TURRET CLASS I AND TURRET CLASS II, J

11、1 POWER CONNECTOR PIN ARRANGEMENT . 16 FIGURE 5 TURRET CLASS I AND TURRET CLASS II, J2 SIGNAL INSERT PIN ARRANGEMENT 19 FIGURE 6 INPUT TIME ROLLOVER PULSE (1 PPS) SIGNAL CHARACTERISTICS . 23 FIGURE 7 TURRET CLASS I AND TURRET CLASS II, J3 VIDEO (COPPER) CONNECTOR INSERT PIN ARRANGEMENT 24 FIGURE 8 T

12、URRET CLASS I AND TURRET CLASS II, J4 FIBER OPTIC INSERT PIN ARRANGEMENT 25 FIGURE 9 TURRET CLASS III, J1 POWER CONNECTOR PIN ARRANGEMENT . 27 FIGURE 10 TURRET CLASS III, J2 SIGNAL INSERT PIN ARRANGEMENT 29 FIGURE 11 TURRET CLASS III, J3 VIDEO (COPPER) CONNECTOR INSERT PIN ARRANGEMENT . 32 FIGURE 12

13、 TURRET CLASS III FIBER OPTIC INSERT PIN ARRANGEMENT 33 FIGURE 13 TURRET CLASS IV, J1 POWER CONNECTOR PIN ARRANGEMENT . 36 FIGURE 14 TURRET CLASS IV, J2 SIGNAL CONNECTOR PIN ARRANGEMENT . 37 FIGURE 15 TURRET CLASS IV, J3 VIDEO (COPPER) CONNECTOR INSERT PIN ARRANGEMENT 39 FIGURE 16 TURRET CLASS IV, J

14、4 FIBER OPTIC INSERT PIN ARRANGEMENT 40 FIGURE 17 TURRET CLASS IV, J5 ADDITIONAL SIGNALS INSERT PIN ARRANGEMENT 41 TABLE 1 ACRONYMS . 8 TABLE 2 SIZES FOR VARIOUS CLASSES 10 TABLE 3 CONNECTOR TYPE AND SIZE FOR VARIOUS TURRET CLASSES . 11 TABLE 4 TURRET CLASS I AND TURRET CLASS II CONNECTORS 12 TABLE

15、5 CLASS I CONFIGURATION CONTROL 13 TABLE 6 CLASS I OPTIONS AND THEIR NAMING CONVENTIONS . 14 TABLE 7 CLASS I CONFIGURATION NAMING EXAMPLES . 14 TABLE 8 CLASS II CONFIGURATION CONTROL . 15 TABLE 9 CLASS II NAMING CONVENTIONS FOR OPTIONS 16 TABLE 10 CLASS II CONFIGURATION NAMING EXAMPLES 16 TABLE 11 T

16、URRET CLASS I AND TURRET CLASS II, J1 POWER CONNECTOR PIN ALLOCATION 17 TABLE 12 TURRET CLASS I J6 AUXILIARY POWER CONNECTOR PIN ALLOCATION 18 TABLE 13 TURRET CLASS I AND TURRET CLASS II, J2 SIGNAL CONNECTOR PIN ALLOCATION . 20 TABLE 14 TURRET CLASS I AND TURRET CLASS II, J3 VIDEO CONNECTOR PIN ALLO

17、CATION . 24 TABLE 15 TURRET CLASS I AND TURRET CLASS II, J4 FIBER OPTIC CONNECTOR PIN ALLOCATION . 25 TABLE 16 TURRET CLASS III CONNECTORS 26 TABLE 17 TURRET CLASS III CONFIGURATION CONTROL 26 TABLE 18 TURRET CLASS III NAMING CONVENTIONS FOR OPTIONS 27 TABLE 19 TURRET CLASS III CONFIGURATION NAMING

18、EXAMPLES . 27 TABLE 20 TURRET CLASS III, J1 POWER CONNECTOR PIN ALLOCATION . 28 TABLE 21 TURRET CLASS III, J2 SIGNAL CONNECTOR PIN ALLOCATION . 29 TABLE 22 TURRET CLASS III, J3 VIDEO (COPPER) CONNECTOR PIN ALLOCATION 33 TABLE 23 TURRET CLASS III, J4 FIBER OPTIC VIDEO CONNECTOR PIN ALLOCATION . 34 TA

19、BLE 24 TURRET CLASS IV CONNECTORS . 34 TABLE 25 CLASS IV CONFIGURATION CONTROL 35 TABLE 26 TURRET CLASS IV NAMING CONVENTIONS FOR OPTIONS . 35 TABLE 27 CLASS IV CONFIGURATION NAMING EXAMPLES . 36 TABLE 28 TURRET CLASS IV, J1 POWER CONNECTOR PIN ALLOCATION 37 TABLE 29 TURRET CLASS IV, J2 SIGNAL CONNE

20、CTOR PIN ASSIGNMENT 38 TABLE 30 TURRET CLASS IV, J3 VIDEO (COPPER) CONNECTOR PIN ASSIGNMENT . 39 TABLE 31 TURRET CLASS IV, J4 FIBER OPTIC CONNECTOR PIN ALLOCATION . 40 TABLE 32 TURRET CLASS IV, J5 ADDITIONAL SIGNALS CONNECTOR PIN ALLOCATION 41 SAE AS6129 Page 3 of 51 1. SCOPE This standard defines a

21、 generic set of electrical interfaces between a host aircraft (“platform”) and an electro-optic/infrared (EO/IR) sensor. This includes connectors, cabling, fiber optics, signals, and power. 1.1 Relationship Between Platform/Sensor Interfaces and SAE AS-1C Standards Figure 1 shows the relationship be

22、tween the various interfaces and the various SAE standards. AS6129 (electrical) covers connectors, conductors and fiber optics signals, and power, and some aspects of data transport. AS6135 (data) covers data (e.g., imagery, metadata, as well as command, status, and response messages.). AS6135 overl

23、aps AS6129 in the area of protocols for data transport. AS6135 and AS6129 are closely bound together because building a system based on these standards is dependent on the requirements from both standards. Also, requirements put in one standard can impact the options for updating the other standard.

24、 NOTE: Regarding Figure 1, SAE is drafting a standard to cover maintenance and test which, if adopted, will likely overlap both AS6129 and AS6135. SAE is also drafting a standard to cover the mechanical interface which, if adopted, will overlap AS6129 with regard to connectors. FIGURE 1 - RELATED SA

25、E STANDARDS 1.2 Purpose The intent of this standard is to enhance interchangeability and interoperability amongst equipment provided by various EO/IR Suppliers and avionic systems. Adoption of this standard will improve procurement flexibility for system integrators and platform providers. Platform

26、providers include fixed wing, rotary wing, UAS (except for micro-UAS) and lighter than air vehicles. The interfaces are designed to facilitate the: a. operation of EO/IR sensor electrical and mechanical subsystems; b. interconnection between EO/IR sensor systems and the avionics systems hosted by th

27、e platform; c. exchange of data and metadata between sensor systems and sensor data processing; d. maintenance of EO/IR systems, allowing for reduction in maintenance equipment in the field and for test. SAE AS6129 Page 4 of 51 1.3 Application This standard applies to all platforms and EO/IR sensors

28、 that interface with each other. AS6129 addresses turreted EO/IR sensor systems. Future revisions of AS6129 may address other classes of EO/IR sensor systems such as non-gimbaled sensors and podded sensors. This standard is intended for application to future sensors and platforms. This includes evol

29、utionary modifications as well as completely new designs. This standard is intended for use by procuring agencies, and as a general guideline for industry. 2. REFERENCES 2.1 Applicable Documents The documents listed in this section are cited in Sections 3 and 4 of this standard. This section does no

30、t include documents cited in other sections of this standard or recommended for additional information or as examples. While every effort has been made to ensure the completeness of this list, document users are cautioned that they must meet all specified requirements of documents cited in Sections

31、3 and 4 of this standard whether or not they are listed here in Section 2. The following publications form a part of this document to the extent specified herein. When specified herein, the specified revision level of a document shall be used. Otherwise, the latest revision level of the specified do

32、cument is implied. 2.1.1 SAE Publications Available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 724-776-4970 (outside USA), www.sae.org. AS50881 Wiring Aerospace Vehicle AS39029/28 Contacts, Electrical Connector, Pin, Crimp

33、Removable, Shielded, Size 12 (for MIL-DTL-38999 Series I, II, III and IV Connectors) AS39029/56 Contacts, Electrical Connector, Socket, Crimp Removable (for MIL-DTL-38999 Series I, III, and IV Connectors) AS39029/58 Contacts, Electrical Connector, Pin, Crimp Removable (for MIL-DTL-24308,MIL-DTL-3899

34、9 Series I, II, III, and IV, and MIL-DTL-55302/69 and MIL-DTL-83733 Connectors) AS39029/75 Contacts, Electrical Connector, Socket, Crimp Removable, Shielded, Size 12 (for MIL-DTL-38999 Series I, III, and IV Connectors) AS85049/80 Connector Accessories, Electrical, Dummy Contact, Sizes 16, 12 and 8,

35、Category 7 (For MIL-DTL-38999 Connectors) 2.1.2 Government Documents Available from http:/www.navcen.uscg.gov/pdf/gps/ICD-GPS-060B.pdf. ICD-GPS-060B GPS User Equipment (Phase III) Interface Control Document for the Precise Time and Time Interval (PTTI) Interface. 12 February 2002 SAE AS6129 Page 5 o

36、f 51 Available from the Document Automation and Production Service (DAPS), Building 4/D, 700 Robbins Avenue, Philadelphia, PA 19111-5094, Tel: 215-697-6257, https:/assist.daps.dla.mil/quicksearch/. MIL-DTL-38999/20G Connectors, Electrical, Circular, Receptacle, Threaded, Wall Mounting Flange, Remova

37、ble Crimp Contacts, Series III, Metric MIL-DTL-38999/24J Connectors, Electrical, Circular, Receptacle, Threaded, Jam-Nut Mounting, Removable Crimp Contacts, Series III, Metric MIL-PRF-29504/4D Termini, Fiber Optic, Connector, Removable, Environment Resisting, Pin Terminus, Size 16, Rear Release, MIL

38、-DTL-38999 Series III MIL-PRF-29504/5D Termini, Fiber Optic, Connector, Removable, Environment Resisting Socket Terminus, Size 16, Rear Release, MIL-DTL-38999 Series III MIL-PRF-39012E Connectors, Coaxial, Radio Frequency, General Specifications for MIL-STD-464 Electromagnetic Environmental Effects,

39、 Reguirements for Systems (01 DEC 2010) MIL-STD-704F Aircraft Electrical Power Characteristics MIL-STD-810G Environmental Engineering Considerration and Laboratory Tests MIL-STD-1560B Insert Arrangements for MIL-DTL-38999 Electrical Circular Connectors MS27488 Plug, End Seal, Electrical Connector 2.

40、1.3 Industry Documents SMPTE ST 292-1:2011 1.5 Gb/s Signal/Data Serial Interface SMPTE ST 297:2006 Television-Serial Digital Fiber Transmission System for SMPTE 259, SMPTE 344, SMPTE 292 and SMPTE 424 Signals SMPTE ST 424:2006 Television-3 Gb/s - Signal/Data Serial Interface TIA/EIA RS-422 TIA(Telec

41、ommunications Industry Association)-422 Electrical Characteristics of Balanced Voltage Differential Interface Circuits IEEE 802.3-2008 IEEE Standard for Information technology Telecommunications and information exchange between systems - Local and metropolitan area networks - Specific requirements -

42、 Part 3: Carrier Sense Multiple Access with Collision Detection (CSMA/CD) Access Method and Physical Layer Specifications ISO/IEC 11801:2002 International Standard: Information technology - Generic cabling for customer premises ICD-GPS-060B GPS User Equipment (Phase III) Interface Control Document f

43、or the Precise Time and Time Interval (PTTI) Interface. 12 February 2002 2.2 Order of Precedence In the event of a conflict between the text of this document and the references cited herein, the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws and

44、 regulations unless a specific exemption has been obtained. SAE AS6129 Page 6 of 51 2.3 Definitions COMMAND, STATUS, AND RESPONSE INTERFACE - Defines the data elements and message sets passed between the host platform and the sensor used to control the operation of the sensor. The protocol for passi

45、ng these messages is handled in co-ordination with the groups which specify the messages. The following types of information are passed through the Command, Status, and Response interface: a. COMMANDS - The set of all digital instructions transmitted to the EO/IR Sensor from the controller which dir

46、ects its operation. These instructions come from an operator, from the platform, or from a pre-programmed set of instructions. These Commands instruct the EO/IR sensor where to point, and which features to utilize in gathering images, such as: slew left; turn on stabilization; lock onto a geo-locati

47、on; change magnification to X; display black as hot versus white hot; turn on image fusion; etc. b. STATUS - Digital information returned from the EO/IR sensor back to the operator, platform, or recorder which provides feedback of sensor operation and other indications of its condition. Examples of

48、this information include: magnification level, azimuth and elevation, stabilization setting, output scale setting for thermal imaging sensors, heading, etc. Another example is the Built-In Test information which might occur periodically, in response to a command, or only if a fault or warning is det

49、ected. Status information can overlap with metadata. c. RESPONSES: Digital information returned from the EO/IR sensor back to the operator, platform, in reply or reaction to a command. Responses are a sub-set of Status. For example, if the command is to turn on stabilization, the response is “stabilization is on”. ELECTRONIC CONTROL UNIT (ECU) - An electronic unit logically between the platform and the sensor, typically inside the platfo