1、L Y MILITARY STANDARD REQUIREMENTS FOR MEMORY LOADERPERIFIER MULTIPLEX BUS INTERFACE WITH AVIONIC SYSTEMS MSC NIA AREA GDRQ DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-
2、,-,-DEPARTMENT OF DEFENSE INTERFACE STANDARD NOT MEASUREMENT I SENSITIVE MIL-STD-2217(AS) NOTICE 2 22 May 2000 MEMORY LOADERNERIFIER MULTIPLEX BUS INTERFACE WITH AVIONIC SYSTEMS, REQUIREMENTS FOR TO ALL HOLDERS OF MIL-STD-2217(AS) 1. THE FOLLOWING PAGES OF MIL-STD-2217(AS) HAVE BEEN REVISED AND SUPE
3、RSEDE THE PAGES LISTED: NEW PAGE DATE SUPERSEDED PAGE DATE 19 22 May 2000 19 16 October 1991 20 16 October 1991 20 Reprinted without change 2. RETAIN THIS NOTICE AND INSERT BEFORE TABLE OF CONTENTS. 3. Holders of MIL-STD-2217(AS) will verify that page changes and additions indicated above have been
4、entered. This notice page will be retained as a check sheet. This issuance, together with appended pages, is a separate publication. Each notice is to be retained by stocking points until the standard is completely revised or canceled. Preparing activity: Navy - AS (Project No. GDRQ-N188) AMSC NIA F
5、SC GDRQ DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-. MIL-STD-22L7 CHG NOTICE L m 97999LL 0428506 581 m NOT MEASUREMENT SENSITIVE MIL-STD-2217(AS) NOTICE 1 28 MAY 1
6、993 MILITARY STANDARD REQUIREMENTS FOR MEMORY LOADERPERIFIER MULTIPLEX BUS INTERFACE WITH AVIONIC SYSTEMS TO ALL HOLDERS OF MIL-STD-2217(AS) 1. The following pages of MIL-STD-2217(AS) have been revised and supersede the pages NEW PAGE 13 14 15 16 75 76 105 106 131 132 147 148 165 166 183 184 listed.
7、 DATE 16 October 1991 28 May 1993 28 May 1993 16 October 1991 28 May 1993 16 October 1991 28 May 1993 16 October 1991 28 May 1993 16 October 1991 28 May 1993 16 October 1991 28 May 1993 16 October 1991 28 May 1993 16 October 1991 SUPERSEDED PAGE 13 14 15 16 75 76 105 106 131 132 147 148 165 166 18 3
8、 184 DATE Reprinted without change 16 October 1991 16 October 1991 Reprinted without change 16 October 1991 Reprinted without change 16 October 1991 Reprinted without change 16 October 1991 Reprinted without change 16 October 1991 Reprinted without change 16 October 1991 Reprinted without change 16
9、October 1991 Reprinted without change 2. RETAIN THIS NOTICE AND INSERT BEFORE TABLE OF CONTENTS. 3. Holders of MIL-STD-2217(AS) will verify that page changes and additions indicated above have been entered. This notice page will be retained as a check sheet. This issuance, together with appended pag
10、es, is a separate publication. Each notice is to be retained by stocking points until the military standard is completely revised or cancelled. Preparing activity: Navy - AS (Project GDRQ-N146) AMSC N/A AREA GDRQ DISTRIBUTION STATEMENT A. Approved for public release, distribution is unlimited. Provi
11、ded by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-2217 GD m 9999911 OLOY777 7 MIL-STD-Z217(AS) DEPARTMENT OF DEFENSE Washington, D.C. 20402 Requirements for Memory Loader/Verifier Mu1 tiplex Bus Interface with Avionic Systems I MIL-STD-2217 1. This
12、mil i tary standard is approved for use by all Bepartments and Agencies of the Department of Defense. 2. Beneficial comments (recommendations, additions, deletions) and any per- tinent data which may be of use in improving this document should be addressed to: Naval Air Development Center Code 5021,
13、 Warminster, PA 18974-5000, by using the self-addressed Standardization Document Improvement Proposal (DD Form 1426) appearing at the end of this document or by letter. ii Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-FORWARD This standard contains
14、 requirements establishing the technical characteristics of the common interface between the AN/ASM-( Memory Loader/Verifier (MLV) and avionic subsystems aboard military aircraft. It defines the interface for all newly developed/modified equipment that uti- lize the MIL-STD-1553 multiplex bus for re
15、programming. This standard does not address any revision to MLV operation with equipment currently reprogrammed this standard will be performed in such a manner as to retain the applicable existing capabilities. For completeness this standard documents the protocol of the MIL-STD-1553 loading techni
16、ques currently in fleet use and makes provisions for adaptation of the common interface to the existing interface. ! o via an MLV. Modifications of existing MLVs to incorporate the provisions of a I iii Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,
17、-MIL-STD-2237 GD m 9979911 0304779 O m MIL-STD-Z217(AS) CONTENTS Page 1 1 1 1 1 2 2 2 2 3 3 3 3 3 3 3 3 3 3 4 4 4 4 4 4 4 4 4 4 4 4 Paragraph 1. SCOPE . 1.1 1.2 1.3 1.4 Scope Interfacing Aircraft. Interfacing Systems . Applicability REFERENCED DOCUMENTS. . 2. 2.1 2.1.1 Government Documents. ., . Spe
18、cifications, Standards and Handbooks . Other Government Documents, Drawings . 2.1.2 and Publications. . Other Publications. . Avail abil i ty of Documents Order of Precedence . . . . . . . . o . . D . . . . . . . . . . . . . . . . . . . . . . 2.2 2.3 2.4 DEFINITIONS . . . . . . . . . . . . 3. . 3.1
19、3.2 3.3 3.4 3.5 3.6 3.7 3.9 3.10 3.11. 3.12 3.13 3.8 Asynchronous. Bit. Bit Rate. . Bootstrap Loading Bus Controller (BC) . Command/Response Mode . DataBus . Message . . . . 8. 8 . Modified Dynamic Bus Allocation Pul se Code Modulation . . . . Remote Terminal (RT) . . Time Division Multiplexing. . W
20、ord. GENERAL REQUIREMENTS. . 4. . 4.1 4.2 4.2.1 4.2.2 Application . Characteristics . Type I Characteristics. Type II Characteristics . . . . . iv Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-T MIL-STD-2217 GD 7477711 010Y780 7 I . CONTENTS . Cont
21、inued . i t 5 . DETAILED REQUIREMENTS 5.1 5.1.1 5.1.1.1 5.1.1.2 5.1.2 5.1.2.1 5.1.2.2 5.1.2.3 5.1.2.4 5.1.2.4.1 5.1.2.4.2 5.1.2.4.3 5.1.2.4.3.1 5.1.2.4,3.1.1 5.1.2.4.3.1.2 5.1.2.4.3.2 5.1.2.4.3.2.1 5.1.2.4.3.2.2 5.1.2.4.3.3 5.1.2.4.3.4 5.1.2.4.4 5.1.2.4.4.1 5.1.2.4.4.2 5.1.2.4.5 5.1.2.4.5.1 5.1.2.4.
22、6 5.1.2.4.7 5.1.2.4.8 5.1.2.4.9 5.1.2.4.10 5.1.2.5 5.1.2.6 5.1.3 5.1.3.1 5.1.3.1.1 5.1.3.1.1.1 5.1,3,1.1.2 Aircraft Subsystem . Power Connector Electrical Characteristics . Mechanical Characteristics . Bus and Discrete Signal Connectors . type I Connection . Type II Connection . Optional Connections
23、 for Redundant Buses . Electrical Characteristics . Primary Data Bus Contacts . Redundant Data Bus Contacts Reprogramming .Enable Di scretes . Reprogramming Enable Types . EW Reprogramming Enable Discretes . AV Reprogramming Enable Di scretes . Reprogram Enable Functions . EW UDM Reprogram Enable Di
24、 screte - Functions . AV Reprgram Enable Discrete Functions Driving the Enable Discretes . i Equipment Timing Aircraft Identification Pins Aircraft Type . Aircraft Configuration Modification . AN/AYK-14 Discretes AN/AYK-14 Discrete Usage Boot Enable Stores Management System (SMS) AN/ALQ-165 External
25、 Processor ON/OFF Discrete . MLV Reserved Pins . F/A-18 Reserved Pins (Type I only) . Associated Ground Pins and Spares . Mechanical Characteristics . F/A-18 Bus and Discrete Signal Connections . Aircraft Wiring Provisions . Electrical Characteristics . Data Bus Characteristics EWMUXBUS . Avionics M
26、UX BUS I, II, III and IV . 7 16 16 16 16 17 17 17 17 17 17 17 17 18 18 18 18 18 20 20 20 20 20 20 20 20 21 21 21 21 27 V Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-2237 GD m 99999LL 0304783 9 m “ MIL-STD-2217(AS) CONTENTS . Continued . 5
27、.1.3.2 5.2 5.2.1 5.2.1.1 5.2.1.2 5.2.1.2.1 5.2.1.2.2 5.2.1.2.3 5.2.1.2.3.1 5.2.1.2.3.2 5.2.2 5.2.2.1 5.2.2.1.1 5.2.2.1.2 5.2.2.1.3 5.2.2.1.3.1 5.2.2.1.3.2 5.2.2.2 5.2.2.2.1 5.2.2.2.2 5.2.2.2.3 5.2.2.3 5.2.2.4 5.2.2.4.1 5.2.2.4.2 5.3 6 . 6.1 6.2 6.3 Figure 1 2 3 4 5 Mechanical Characteristics . MLV S
28、ubsystem . MLV Description Power Cable Bus and Discrete Signal Cable . MLV Bus Connection . MLV Discrete Connections Nomenclature Conventions . . e . . Multiplex Buses RS-422 Interface MLV Operation . MLV Preparation . MLV Operating Software . Library File Memory Files Lookup Table Reprogramming Dat
29、a . Initial On-Line Operations . Automatic Reprogram Operation . Manual Reprogram Operation . MLV Control of AN/AYK-14 (Automatic Avionics Subsystem Memory Load-Verify . Final On-Line Operations Bus Processing Completion . Aircraft Processing Completion . Avionic Equipment Requirements . and Manual
30、Reprogram Operation) 27 27 27 28 28 28 28 28 6 28 28 30 30 30 30 32 32 33 33 35 37 40 38 e 40 40 41 41 NOTES 41 Lookup Table Data . 41 Flow Chart Notation 49 Subject Term (Key Word) Listing 49 F I GURES Type I Interface Connection Diagram . 5 Type II Interface Connection Diagram . 6 Generalized Airc
31、raft Cabling Schematic for Type I Interface Connection 23 General i zed Aircraft Cab1 ing Schematic for Type II Interface Connection 25 Bus Coupling Methods . . . . 29 vi Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-6 7 8 9 10 11 12 13 14 15 16 17
32、 18 Tab1 e I II III IV V VI VI I FIGURES - Continued. Bus Control Initiation/Final On-Line Operations. 51 Word Formats. 54 Bus Controller to Remote Terminal Data Transfer. . 57 Remote Terminal to Bus Controller Data -Transfer. . 58 Avionics Subsystem = RT Load/Verify Procedure . 60 Avionics Subsyste
33、m = BC LoadlVerify Procedure . 92 AN/AYK-14 SIM-B = RT Load/Verify Procedure . 122 AN/AYK-14 SIM-B = BC Load Procedure . 140 F/A-18 SMS/SDC Load Procedure 155 F/A-18 SMS/SDC Verify Procedure . 157 AN/AYK-14 SIM-A Load Procedure. . 176 CP-1001 Load Procedure. . 190 CP-1001 Verify Procedure. 192 TABLE
34、S Power Connector J1 Pin Designation for Type I and Type II Interface Connection. 8 Bus and Discrete Connector J2 Pin Designations for Type I Interface Connection. 9 Designations for Type I Interface Connection. 11 Discrete Connector J2 Pin Designations for Type II Interface Connection. . , 12 Bus C
35、onnectors J3 and J4 Contact Designations for Type II Interface Connection. 14 Designations for Type II Interface Connection, 15 Aircraft Type Code. . 19 Redundant Bus Connector J3 Pin Redundant Bus Connector J5 Contact vi i Provided by IHSNot for ResaleNo reproduction or networking permitted without
36、 license from IHS-,-,-Paragraph Paragraph APPENDICES APPENDIX A 10 . 10.1 10.1.1 10.1.2 10.1.3 10.2 10.2.1 10.2.2 APPENDIX B 20 . 20.1 20.2 20.3 20.4 20.4.1 20.4.1.1 20.4.1.1.1 20.4.1.1.2 20.4.1.2 20.4.1.2.1 20.4.1.3 20.4.2 .20.4. 2.1 20.4.2.1.1 20.4.2.2 20.4.2.2.1 20.4.2.2.2 20.4.3 20.4.3.1 20.4.3.
37、1.1 20.4.3.2.1 20.4.3.2.2 20.4.3.2.3 20.4.3.2; BUS PROTOCOL . MESSAGE TRANSFER Word Types . Command Word Format Status Word Format . Data Word Format Message Formats BC to RT Transfer Sequence . RT to BC Transfer Sequence . MESSAGE FORMATS MLV = BC . STANDARD PROTOCOL FOR REMOTE. . TERMINALS Applica
38、bility . General Operation . Status Response Word: MLV = BC Messages Activity: MLV = BC: TR = 1: SUBADDRESS = 07H . Activity Message Bus Data . Activity Message Utilization Status Ward Data Words . Data Word1 Activity .Messages Prior to Beginning a Load/Veri fy or Verify . Memory Configuration: MLV
39、= BC: TR = 1: SUBADDRESS = 13H Memory Configuration Bus Data . Memory Configuration Message Utilization . Data Words . Data Word 1 . DataWord2 Reprogram Control : MLV = BC : TR = O: Reprogram Control Bus Data. Reprogram Control Message Utilization . Data Words . Dataword1 Data Word 2 Data Word 3 , S
40、UBADDRESS = 1DH 53 53 53 53 55 56 56 . 56 56 59 59 59 59 62 65 “ 65 66 66 66 68 68 69 69 69 69 70 70 71 71 71 71 71 viii Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-. S 20.4.3.2.4 20.4.3.2.4.1 20.4.3.2.4.1.1 20.4.3.2.4.1.2 20.4.4 20.4.4.1 20.4.4.
41、1.1 20.4.4.2 20.4.4.2.1 20.4.4.2.2 20.4.4.2.3 20.4.4.2.4 20.4.5 20.4.5.1 20.4.5.1.1 20.4.5.1.1.1 20.4.5.2 20.4.6 20.4.6.1 20.4.6.1.1 20.4.6.1.1.1 20.4.6.2 20.4.7 20.4.7.1 20.4.7.1.1 20.4.7.2 20.4.7.2.1 20.4.7.2.2 20.4.8 20.4.8.1 20.4.8.1.1 20.4.8.2 20.4.8.2.1 20.4.9 20.4.9.1 20.4.9.1.1 20.4.9.2 20.4
42、.9.2.1 Appendix B . Continued . Data Word 4 71 Control Code Processing 72 Field Validity . 72 Valid Control Codes 72 Header : MLV = BC: TR = O : SUBADDRESS . = .14 H. 74 Header Bus Data . 74 Header Message Utilization . 75 Data Words . 75 Data Word 1 75 Data Word 2 76 Data Word 3 76 Data Word 4 76 .
43、 Memory Data Load: MLV = BC: TR = O: SUBADDRESS = 15H . 78 Memory Data L0a.d Bus Data . 78 Memory Data Load Message Utilization . . 79 BUSY Bit 79 Data Words . 79 Memory Data Verify : MLV = BC : TR = 1 : SUBADDRESS = 15H . 80 Memory Data Verify Bus Data 80 Memory Data Verify Message Utilization . 81
44、 BUSY Bit 81 Data Words . 81 Trailer: MLV = BC: TR = O: SUBADDRESS = 16H . 82 Trailer Bus Data 82 Trailer Message Utilization 83 Data Words. 83 Data Word 1 83 Data Word 2 83 Reprogram Status: MLV = BC: TR = 1: SUBADDRESS = 17H . 85 Reprogram Status Bus Data . 85 Reprogram Status Message Utilization
45、. . 86 Data Words . 86 Data Word 1 . 86 MLV Error : MLV = BC: TR = O: SUBADDRESS = 17H . 88 MLV Error Bus Data . 88 MLV Error Message Utilization . 89 Data Words . 89 Data Word 1 89 ix Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-! . Appendix C AP
46、PENDIX C MESSAGE FORMATS MLV = RT . 91 Paragraph 30 . 30.1 30.2 30.3 30.4 30.4.1 30.4.1.1 30.4.1.1.1 30.4.1.1.2 30.4.1.2 30.4.1.2.1 30.4.2 30.4.2.1 30.4.2.1.1 30.4.2.2 30.4.2.2.1 30.4.2.2.2 30.4.3 30.4.3.1 30.4.3.1.1 30.4.3.2 30.4.3.2.1 30.4.3.2.2 30.4.3.2.3 30.4.3.2.4 30.4.3.2.4.1 30.4.3.2.4.1.1 30
47、.4.3.2.4.1.2 30.4.4 30.4.4.1 30.4.4.1.1 30.4.4.2 30.4.4.2.1 30.4.4.2.2 30.4.4.2.3 30.4.4.2.4 30.4.5 STANDARD PROTOCOL FOR BUS CONTROLLERS 91 Applicability . 91 General Operation . . . 91 Status Response Word: MLV = RT 94 Messages . . . . . . . 96 Activity Message: MLV = RT: TR = 1: SUBADDRESS = 07H
48、. 96 Activity Message Bus Data . . . . 96 Activity Message Utilization 96 Status Word 96 Data Words 97 Dataword1 97 Memory Configuration: MLV = RT: TR = O: SUBADDRESS = 13H . . 98 Memory Configuration Bus Data . . 98 Memory Configuration Message Utilization . 99 Data Words . 99 Data Word 1 99 DataWo
49、rd2 99 Reprogram Control : MLV = RT: TR = 1: SUBADDRESS = 1DH . 100 Reprogram Control Bus Data . 100 Reprogram Control Message Utilization 101 Data Words . 101 DataNordl 101 Data Word 2 101 DataWord3 101 DataWord4 101 Control Code Processing 102 Field Validity . 102 Valid Control Codes 102 Header: MLV = RT: TR = 1: SUBADDRESS = 14H . 104 Header Bus Data 104 Header
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