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Site Monitor Demonstrator
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1. BDS normal update 54 0 Maximum update time 284 4 Figure no 4 ARINC transmitter permanent data flow More than 60 of the transmitter time is available for data link The firmware architectural design and functional description are not included in this document but can be supplied by EUROCONTROL Site Monitor Demonstrator 7 Tals 7 2 Site Monitor Demonstrator User Manual Introduction The purpose of this chapter is to give a general overview of how a user can install and implement this software package and at the same time to describe how to use all the SMD software facilities Installing the Site Monitor Demonstrator The SMD software is archived in the file site tar In the subdirectory users jma site use the command tar xvf site tar to extract all related files In the subdirectory site site bin execute the file make0 to compile the source files which are located in the subdirectory site site src After successful compiling the following executable files should be found sitemain Main process sitefldat Flight data monitor siteaac AAC interface siteup Uplink driver sitedown Downlink driver sitedownmon Downlink monitor siteupmon Uplink monitor siteuser User main interface site File script to start running the SM sitegigen GICB generation sitegiedit GICB editor sitegimon GICB monitor gicb dat Default file with A
2. FLIGHT ALTITUDE min value of 43000 ft Confirm it by typing y Y or ENTER To cancel it type N or n 7 4 2 1 2 High Security Level To chose this option type function key F2 To proceed a password must be enter Type ENTER to finish WRITE PASSWORD If an incorrect password is entered the following message will be displayed and the process will return to the main menu SORRY BUT YOU HAVE A WRONG PASSWORD TRY AGAIN If a correct password is entered complete the following displayed table Type ENTER to finish HIGH SECURITY LEVEL FLIGHT ALTITUDE CONTROL WORD CODE 4 octal char FLIGHT IDENTIFICATION max 8 alfan char Confirm it by typing y Y or ENTER To cancel it type N or n Site Monitor Demonstrator 14 7 4 2 1 3 Change Password To chose this option type function key lt F3 gt Complete the following displayed table WRITE OLD PASSWORD If an incorrect password is introduced the following message will be displayed and the process will return to the main menu SORRY BUT YOU HAVE A WRONG PASSWORD TRY AGAIN If a correct password is introduced complete the following displayed table with the new password WRITE NEW PASSWORD max 8 alfan char Confirm it by typing y Y or ENTER To cancel it type N or n T
3. messages flight identification altitude and control word This part was written in HP UX C programming language Since the application is running in a HP UX operating system it became necessary to implement a HP UX driver to access the card This driver developed by Hewlett Packard France can be configured accordingly with the chosen AAC interrupt level and memory address The configuration manual of this driver is not included in this document but can be supplied by EUROCONTROL Finally the low level software running in the card the firmware implementing the high speed ARINC 718 4 and the low speed 429 14 5 For the firmware the following considerations about time and load processing can be made The DLPU ADLP of the SMD has to answer a RTS from the transponder within 4 0 milliseconds with a CTS The answer may be delayed by 2 88 milliseconds if a low speed broadcast word has to be sent The normal reaction time of the ARINC card to answer a RTS with a CTS is on average 0 7 milliseconds So the worse case delay for a CTS is 3 58 milliseconds which is less than 4 0 milliseconds There is only one ARINC transmitter with 4 multiplexed drivers and all information has to go through this transmitter The following table shows the permanent data flow of the transmitter in milliseconds per second Transmitter occupancy Control word update 86 4 Altitude update 86 4 Flight identification update 57 6
4. COMM D MESSAGE WITH 10 SEGMENTS TEST ELM COMM D MESSAGE WITH 10 SEGMENTS vr THIS IS A DOWNLINK MESSAGE FOR TESTING AN ELM WITH 16 SEGMENTS WITH APN 1 THIS IS A DOWNLINK MESSAGE FOR TESTING AN ELM WITH 16 SEGMENTS WITH APN 1 AFR405 REQUEST FL345 AT NANTES WAYPOINT SAB546 REQUEST DIRECT ROUTING ON FL240 AT PARIS ORLY TAP420 REQUEST METEO REPORT FOR EDDF LUF345 REQUEST ATIS INFORMATION FOR LPPO BRI345 REPORTING CB TURBULENCE AT FL300 THY345 REPORTING UFO AT BRETIGNY REGION AFR345 REPORTING ALL FREQUENCIES OFF LINE INCLUDING EMERGENCY 119 15 TEST MESSAGE Site Monitor Demonstrator 16 1 2 4 5 6 7 REQUEST VOLMET AT ZONE LFPG REQUEST TAF AT ZONE LFPG REQUEST METAR AT ZONE LFPG REQUEST PRELDG AT ZONE LFPG REQUEST SIGMET AT ZONE LFPG REQUEST ATIS INFORMATION LFPG REQUEST ATIS INFORMATION FROM LFPG LFLY All the messages activated by a function key are phrase coded 6 These messages examples were used in PARIS region The file mes txt contain also the downlink radar identification which is on line modifiable The format is pr opepwiT E rT E vjefA T o N x x x x x Downlink radar identification use decimal char max 16 min 1 7 4 2 3 Quit Site Monitor Demontrator To chose this option type function key lt F3 gt Confirm it by typing lt y gt lt Y gt or ENTE
5. Demonstrator 9 7 4 Site Monitor Demontrator Operating Instructions 7 4 1 GICB Editor The GICB editor is an on line editor of simulated AVIONICS data Data can be introduced having as parameters the BDS number the resolution and the minimum and maximum value accepted BDS DATA RANGE RESOLUTION 5 Airborne Format 0 7 14 Surveillance Status Q 3 Turn Indicator Bit 0 1 Barometric Altitude 50 175 ft 25 ft Time Bit 01 Latitude 4 90 0 0007 Longitude 180 0 0014 6 Type 5 5 6 Movement MOV_SPM 0 128 Track 180 2 816 Barometric Altitude 50 175 ft 25 ft Time Bit 0 1 Latitude 4 90 0 0007 Longitude 180 0 0014 10 Capability Report Use hexadecimal data to fill 20 Aircraft Identification Defined in the user main interface Flight Data lt F1 gt 30 Reserved for ACAS Use hexadecimal data to fill Site Monitor Demonstrator 10 BDS DATA RANGE RESOLUTION 40 Flight Path Angle 180 0 18 Flight Path Acceleration 4g 0 001 g Corrected Angle of Attack 180 0 044 Barometric Correction Altitude 131 072 ft 8 ft 50 Mach Number 4 096 Mach 0 001 Mach Computed Air Speed 1 024 Kt 0 5 Kt Track Angle True 180 0 044 Track Angle Magnetic 180 0 044 60 Track Angle Magnetic 180 0 044 Ground Speed 2 048 Kt 0 5 Kt Altitude Rate 16 384 ft min 64 ft min Stat
6. EUROPEAN ORGANISATION FOR THE SAFETY OF AIR NAVIGATION Ty EUROCONTROL EUROCONTROL EXPERIMENTAL CENTRE SITE MONITOR DEMONSTRATOR EEC Note No 28 96 EEC Task C07 EATCHIP Task SUR 3 Issued December 1996 The information contained in this document is the property of the EUROCONTROL Agency and no part should be reproduced in any form without the Agency s permission The views expressed herein do not necessarily reflect the official views or policy of the Agency REPORT DOCUMENTATION PAGE Reference Security Classification EEC Note No 28 96 Unclassified Originator Originator Corporate Author Name Location EEC COM EUROCONTROL Experimental Centre Communication B P 15 P F 91222 Br tigny sur Orge CEDEX FRANCE Telephone 33 1 69 88 75 00 Sponsor Sponsor Contract Authority Name Location EATCHIP Development Directorate EUROCONTROL Agency Rue de la Fus e 96 B 1130 BRUXELLES Telephone 32 2 729 9011 TITLE SITE MONITOR DEMONSTRATOR Authors Date Pages Figures Photos Appendix References 12 96 iv 18 4 2 0 6 Hans P ENGLMEIER Joao M M MARTINS EATCHIP Task EEC Task No Task No Sponsor Period Specification SUR 3 C07 4 96 to 11 96 Distribution Statement a Controlled by Head of COM b Special Limitations None c Copy to NTIS YES NO Descriptors keywords Mode S Subnetwork Aircraft Equipment Simulation ARINC Protocols Site Moni
7. R To cancel it type lt N gt or n 7 4 3 Final Considerations All the other processes do not require any user operation Site Monitor Demonstrator 17 1 2 3 4 5 6 References EEC Note No 17 94 Advanced PC ARINC Card version 2 by H P ENGLMEIER EEC Note No 26 95 Remote Transponder by H P ENGLMEIER EEC Note No 16 95 Test Data Link Processor UNIX version by H P ENGLMEIER and J M Mateus Martins ARINC Document Mark 3 Air Traffic Control Transponder ATCRBS Mode S ARINC Characteristic 718 4 15 12 1989 ARINC Document Mark 33 Digital Information Transfer System ARINC Characteristic 429 12 1 7 1990 User Manual for TUB Software in DLPU Model C2 01 11 1992 by M Lehmensiek Site Monitor Demonstrator 18 cs rl Pee cu ien EE pni es EEC December 1996 hy H P Koglmeier and Joso M Mortins D Ei El i 1 7 UL PUN pits ap arr iN rhe path scegtezation range dg en D 0019 tore ud 180 0 0 0044 Baro Spa ie EE cotati eC computed air spend range LOB res 0 St eite esie nete pr eem SITE R GENERATOR
8. VIONICS data sem ftok site shm ftok site IPC semaphores facilities reference file IPC shared memory facilities reference file AAC firmware Site Monitor Demonstrator 7 3 Note All screen output messages are recorded in a file with extension rec The complete list of files necessary to run the SMD should also include the HP UX driver necessary to establish the connection between the AAC firmware and this software application Running the Site Monitor Demonstrator To start running the user should type site This script file before activating the 11 processes mentioned below asks the name of the GICB file used If nothing is written after having pressed lt ENTER gt key the file gicb dat is read by default see Photo1 Each of the 11 processes activated are running in a single hpterm visual window see Photo 2 SITE FLIGHT DATA MONITOR gt sitefldat SITE DOWNLINK DRIVER sitedown SITE UPLINK DRIVER sgiteup SITE DOWNLINK MONITOR gt sitedownmon SITE UPLINK MONITOR siteupmon SITE AAC INTERFACE giteaac SITE USER MAIN INTERFACE gt siteuser SITE_MAIN_PROCESS sitemain SITE_GICB_GENERATOR sitegigen SITE_GICB_EDITOR sitegiedit SITE_GICB_MONITOR sitegimon Use the mouse to select the correspondent hpterm window How to operate with all processes will be described in the next chapter Site Monitor
9. are to be developed In the moment the SMD is compatible with actual used DLPU but in a near future it must be slightly modified to be compatible with the ADLP This is due to the implementation of the GDLP Site Monitor Demonstrator 5 6 Site Monitor Demonstrator Software Architectural Design 1 Uplink 2 User 3 Downlink 4 GICB Monitor Interface Monitor Editor F2 5 Uplink 6 Main 7 Downlink 8 GICB Driver Process Driver Generator F9 10 9 AAC Flight Data 11 GICB Interface i Monit High Level Monitor onitor SMD part Site Monitor Demonstrator installed in a HP UX workstation Advanced 13 AAC Arinc Card Firmware version 2 board Low Level SMD part ARINC 718 Bus ARINC 429 Bus Figure no 3 SMD software architectural design Notes 1 F1 to F10 are System V IPC facilities shared memory and semaphores 2 NO to N2 are HP UX kernel data transfer blocks 3 AO and 1 are ARINC channels Site Monitor Demonstrator 6 As shown above the SMD is basically an upgraded version of the UNIX based TDLP 3 This software device can be split in three parts the high level running in the HP UX workstation the HP UX driver to access the AAC and finally the low level software running in the card the firmware The high level part performs the following tasks AAC driver interface user interfacing for editing downlink messages GICBs generation and finally data link monitoring including surveillance
10. ator 12 BDS DATA RANGE RESOLUTION 17 N1 Actual Engine 1 256 rpm 0 13 rpm Fuel Flow Engine 1 32 768 lb hr 8 Ib hr Total Air Temperature 512 0 5 Static Air Temperature 512 0 5 27 N1 Actual Engine 2 256 rpm 0 13 rpm Fuel Flow Engine 2 32 768 lb hr 8 Ib hr Total Air Temperature 512 0 5 Static Air Temperature 512 0 5 37 N1 Actual Engine 3 256 rpm 0 13 rpm Fuel Flow Engine 3 32 768 lb hr 8 Ib hr Total Air Temperature 512 0 5 Static Air Temperature 512 0 5 47 N1 Actual Engine 4 256 rpm 0 13 rpm Fuel Flow Engine 4 32 768 lb hr 8 Ib hr Total Air Temperature 512 0 5 Static Air Temperature 512 0 5 1 Aircraft Identification 2 char ISO5 Label 233 Aircraft Identification 2 char ISO5 Label 234 Aircraft Identification 2 char ISO5 Label 235 1B Aircraft Identification 2 char ISO5 Label 236 Site Monitor Demonstrator 13 7 4 2 Main User Interface This process allows the user to terminate a session and to edit or to send downlink messages including aircraft flight data 7 4 2 1 Flight Data To chose this option type function key lt F1 gt 7 4 2 1 1 Low Security Level To chose this option type function key lt F1 gt and complete the following displayed table Type lt gt to finish LOW SECURITY LEVEL FLIGHT IDENTIFICATION max 8 alfan char
11. ececeeeeaas 9 7 4 SITE MONITOR DEMONTRATOR OPERATING 5 10 LATE GI CB EUON e ete Ra 7 4 2 Main User Interface PALA Elight DGG svag ede deti ede aes diae 7 4 2 1 1 Low Security Level idee eee eer bett 14 74 2 1 2 High Security Level 5 5 nescit ditti deett ederet 14 7 4 2 1 3 Change Password deinde dee teneo dee Ht eee Ede t 6 saal sb enero pede edens 15 TA D2 Downlink Messtes te k 15 F422 b On Line Messages iso d P e DR EE RETE Ce Eee e eb R 15 7 4 2 2 2 Predefined Messa p sa a etsi t eth t ai oe deed E eene ege lea dst 15 7 4 2 3 Quit Site Monitor Demontrator 17 4 4 3 Final Consid EdflOWss 5 5 cose cede sti edet te E ak eade A t A R 17 1 1 2 2 Site Monitor Demonstrator iv 1 Acronyms and Abbreviations Definitions AAC ACAS ADLP ATN BDS CTS DLPU ELM GDLP GICB IIMSES RTS SLM SMD SNTF TUB XPDR Advanced ARINC Card Aircraft Collision Avoidance System Aircraft Data Link Processor Unit Aeronautical Telecommunication Network Binary Data Store Register number with 56 bit in the Mode S transponder Clear to send Data Link Processor Unit Extended Length Message Ground Data Link Processor Ground Initiated Comm B Messages Initial Implementation Mode S in Enhanced Surveillance Request to send Short Length Message Site M
12. generate flight identification control word and flight altitude broadcast messages using an ARINC 429 protocol 5 General Overview ARINC 718 caring Mode S Messages ARINC 429 caring Zlir 1 Flight Identification Control Word Flight Altitude Figure no 2 General overview of a SMD environment There are two differences between normal grounded aircraft equipment and the SMD The first is a delay line installed in a parrot transponder near the radar to put it at a longer distance 2 The second is the existence of a special device a DLPU or a ADLP which can also execute the functions of the transponder control box and the altimeter This device can be realised by a workstation with a PC ARINC card 1 Installed in a network environment it can be used in a remote mode The ARINC card has two receivers and 4 multiplexed transmitters It uses a Harris ARINC processor which allows different transmission speeds for reception and transmission Site Monitor Demonstrator 4 Two high speed receivers and two high speed transmitters are used for the ARINC 718 interface between the American transponder and the SMD The two remaining transmission channels are used in the following way one for the transmission of the control word channel 3 and the other for the transmission of the altitude and flight identification channel 4 Both channels use low speed transmi
13. he new password will be written in file paswrd txt 7 4 2 2 Downlink Messages To chose this option type function key F2 7 4 2 2 1 On Line Messages To chose this option type F1 Complete the following displayed table and type ENTER to finish Confirm it by typing y Y or lt ENTER gt The maximum size of each message is 208 characters which corresponds to a COMD of 16 segments mode atc and 6 bit code 6 DOWNLINK MESSAGE 208 alfan char If you want to send this message more then once confirm it by writing the corespondent number For a single time type ENTER or lt 1 gt To quit type lt 0 gt 7 4 2 2 2 Pre defined Messages The file mes txt contain all the pre defined messages These messages can be on line written or modified The general format for these messages is tact REL Site Monitor Demonstrator 15 ELE In file Start message indicator Message number decimal char or function key Message number decimal char or function key Space Message alph char Stop message indicator mes txt there are already 15 messages They can be activated by typing the corresponding number as follows 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 COMB COMMB LINKED 2 TEST COMM B LINKED 3 TEST COMM B LINKED 4 SES TEST ELM
14. ic Air Temperature 512 0 5 70 Selected Altitude Range 65 536 ft 16 ft Selected Heading 180 0 8 Status Word 1 270 Binary Input Status Word 2 271 Binary Input 80 Selected Airspeed 512 Kt 0 25 Kt Selected Altitude Rate 16 384 ft min 16 ft min Selected Altitude 45 536 ft 16 ft Status Word 1 Label 270 Binary Input 90 Selected Mach Number 4 096 Mach 0 002 Mach Selected Altitude Rate 16 834 ft min 16 ft min Selected Altitude 65 536 ft 16 ft Status Word 2 Label 271 Binary Input AO Cross Track Error 128 nm 0 004 nm Vertical Deviation 2 048 ft 1 ft Acceleration 19 0 0169 BO Computer Airspeed 1 024 Kt 0 25 Kt True Airspeed 2 048 Kt 0 5 Kt Mach 4 096 Mach 0 00025 Mach Heading magnetic 180 0 18 Site Monitor Demonstrator 11 BDS DATA RANGE RESOLUTION CO Radio Height 8 192 ft 1 ft Average Static Pressure 1 024 mb 0 25 mb Altitude 131 072 ft 1 ft 31 Bearing to Waypoint 180 0 18 Time to Go 399 9 min 0 1 min Distance to go 399 9 nm 0 1 nm 41 Active Waypoint 1 3 characters ISO 5 Active Waypoint 2 3 characters ISO 5 Desired Track 180 0 18 51 Latitude 90 0 00035 Longitude 180 0 0007 Altitude 131 072 ft 8 ft 61 G M T HHMMSS Flight Number XXXX 71 Roll Angle 90 0 35 Altitude Rate 8 192 ft min 128 ft min Wind Speed 256 Kt 1 Kt Wind Angle 180 0 703 24 Centre of Gravity 99 9 0 1 96 Gross Weight 131 072 lbs 160 Ibs Site Monitor Demonstr
15. onitor Demonstrator Sub Network Test Facility Technische Universitat Braunschweig Mode S Transponder Site Monitor Demonstrator 2 Purpose and Scope The purpose of this document is to provide an overall description of the software architectural design and user manual of the Site Monitor Demonstrator test tool developed at the EUROCONTROL Experimental Centre 3 Introduction The Site Monitor Demonstrator is part of the IIMSES programme and is a test tool for the radar stations involved in this programme This will be an industrial product the EEC produces it only as a demonstrator Site Monitor Demonstrator 2 4 Major Features of the Site Monitor Demonstrator Site Monitor Demonstrator GICB EDITING GICB GENERATION DATA LINK MONITORING CONTROL WORD EDITING and GENERATION ARINC 718 PROTOCOL GENERATION Figure no 1 Major features of the Site Monitor Demonstrator The Site Monitor Demonstrator test tool is a software device Installed in a HP UX MESSAGES EDITING DOWNLINK MESSAGES GENERATION FLIGHT IDENTIFICATION EDITING and GENERATION FLIGHT ALTITUDE EDITING and GENERATION ARINC 429 PROTOCOL GENERATION workstation and using an Advanced ARINC Card version 2 1 Site Monitor Demonstrator The SMD software has two major functionalities The first is the capacity of generate and monitor Mode S data link messages using an ARINC 718 protocol and the second is the capacity of
16. ssion The firmware on the AAC can implement a single ARINC 718 channel with the transponder or a double The software of the workstation is an upgraded version of TDLP including control box and altimeter functions In the EEC Mode S avionics test chain a switch is installed to take the ARINC 429 broadcast for control word altitude and flight identification either from the control box and altimeter or from the SMD The objective of the site monitor is to allow a radar operator or the ground control the variation of all aircraft parameters sent to the parrot transponder including control word altitude and flight identification Further all data link applications must be available for test purposes including special cases as the transmission of 10 COMM B between two radar beam hits and verify whether the transponder has lost any data Users for the site monitor are radar constructors and radar users It is not excluded that the material of the EEC delay lines and ARINC cards will be used for the industrial SMD production The SMD is a simple test tool and has nothing to do with the end to end test chain for data link applications foreseen in the ATN program the Sub Network Test Facility SNTF Nevertheless the SMD upgraded by an interface to the GDLP could be a part of the end to end test chain mention above If this option is accepted the workstation of the SMD could house the softw
17. tor Demonstrator HP UX Environment Remote Access Advanced ARINC Card HP UX C Abstract This report describes the software architectural design and user manual of the Site Monitor Demonstrator This document has been collated by mechanical means Should there be missing pages please report to EUROCONTROL Experimental Centre Publications Office B P 15 91222 BRETIGNY SUR ORGE CEDEX France EEC Note No 28 96 EEC Task No C07 EATCHIP Task No SUR 3 Issued December 1996 Site Monitor Demonstrator by Hans Peter ENGLMEIER and Jo o Manuel MATEUS MARTINS EUROCONTROL Experimental Centre Summary This report describes the software architectural design and user manual of the Site Monitor Demonstrator Site Monitor Demonstrator iii CONTENTS 1 ACRONYMS AND ABBREVIATIONS DEFINITIONS aaansentantestansansannnnnnsannunnnnnannnnnnnnannnnnannan aa 4 MAJOR FEATURES OF THE SITE MONITOR DEMONSTRATOR asansntestestentansansannnnnnsannnnnn 2 6 SITE MONITOR DEMONSTRATOR SOFTWARE ARCHITECTURAL DESIGN 6 7 SITE MONITOR DEMONSTRATOR USER MANUAL 2k2aana ntsstestansannannnnnnnnnnnnnnnnnnnannnnnnnnnnnannn n a m m O Je INTRODU GTION ee 8 7 2 INSTALLING THE SITE MONITOR DEMONSTRATOR 8 7 3 RUNNING THE SITE MONITOR DEMONSTRATOR ccccccssssesecccceeeceessssssceecccceseuaesseecccesscuuanseecceeseseuanee
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