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Vislink ADVENT DCU5000, Operation Handbook

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Advent Communications 

WARNINGS AND HAZARDS 

Failure to operate and use the equipment other than instructed in the 
manual may result in ELECTRIC SHOCK. 

 

HAZARDOUS WARNING LABELS 

  

Hazardous AC voltages present 

 

NON-IONISING RADIATION 

 

Possible source of radiation hazard, normally located 
at waveguide connections, waveguide joints and 
antennas. 

 

CAUTION – HEAVY ITEMS 

 

Some items of equipment may weigh in 
excess of 25kg, do not attempt to move 
or lift without assistance 

 

CAUTION – MOVING PARTS 

  

During operation of the antenna there 
will be moving parts; do not touch 
whilst in motion 

 

209297 – DCU5000 Drive Control Unit 

Page 4 of 42 

Summary of Contents for ADVENT DCU5000

Page 1: ...e copied used or disclosed to others for any purpose except as authorised by Advent Communications ADVENT COMMUNICATIONS Preston Hill House Nashleigh Hill Chesham Bucks HP5 3HE England Telephone National 01494 774400 Fax 01494 791127 24 Hour Support International 44 1494 810410 E Mail support adventcomms com ADVENT DCU5000 DRIVE CONTROL UNIT ...

Page 2: ...Advent Communications 209297 DCU5000 Drive Control Unit Page 2 of 42 AMENDMENT RECORD SHEET ISS DATE ECR PAGE DESCRIPTION A 01 03 07 Initial release B 12 08 08 Correction to F20 alarm description ...

Page 3: ...Advent Communications EMC DECLARATION 209297 DCU5000 Drive Control Unit Page 3 of 42 ...

Page 4: ...N IONISING RADIATION Possible source of radiation hazard normally located at waveguide connections waveguide joints and antennas CAUTION HEAVY ITEMS Some items of equipment may weigh in excess of 25kg do not attempt to move or lift without assistance CAUTION MOVING PARTS During operation of the antenna there will be moving parts do not touch whilst in motion 209297 DCU5000 Drive Control Unit Page ...

Page 5: ...TECTED 14 4 8 F7 FREEWHEEL DETECTED 15 4 9 F8 END OF TRAVEL DETECTED 15 4 10 F9 TX POL SWITCH FAILED 15 4 11 F10 AZIMUTH STOW SENSOR FAILED 15 4 12 F11 ELEVATION STOW SENSOR FAILED 15 4 13 F12 POL STOW SENSOR FAILED 15 4 14 F13 EL DP SENSOR FAILED 15 4 15 F14 FA DP SENSOR FAILED 15 4 16 F15 EL STOWED SENSOR FAILED 15 4 17 F16 FPGA PROGRAMMING FAILED 16 4 18 F17 MANUAL BRAKE OVERRIDE ON 16 4 19 F18...

Page 6: ... PROM CHECKSUM ERROR 18 4 52 F52 SOFTLIMIT DATA ERROR 18 4 53 F53 WOODED AREA DATA ERROR 19 4 54 F54 CAL AREA DATA ERROR 19 4 55 F55 FPGA COMPATIBILITY WARNING 19 4 56 F56 EXT FLASH ERROR 19 4 57 F58 HEATSINK FAN STALL DETECTED 19 4 58 F59 HMR3300 TEMPERATURE WARNING 19 4 59 F60 HMR3300 TEMPERATURE ALARM 19 4 60 F61 F64 ALARM ERROR 19 5 REMOTE CONTROL 20 5 1 INTRODUCTION 20 5 2 SET UP 20 5 3 PACKE...

Page 7: ... the current Advent range of motorised antennas The unit is a 1U high half width 360mm deep chassis and is mains powered 90 264V AC 47 63 HZ 100VA The DCU5000 has a RS485 serial communications interface allowing the unit to be controlled using a SatFinder ACU4XXX or ACU5XXX to implement the autoSearch and autoTrack control of an antenna system ...

Page 8: ...nsions Half width 1U chassis x 360 mm deep Weight 2 0 kg approx Power Connector 3 Pin IEC plug with dual fusing AC Supply 90 264V AC 47 63Hz Consumption 100VA Temperature Range 20 to 50 C operating 40 to 80 C storage 2 2 ANGULAR POSITIONAL DISPLAY Azimuth 0 1 Elevation 0 1 Polarisation 0 1 2 3 ANGULAR CONTROL The maximum angular rates are determined by the antenna type and version the DCU5000 is c...

Page 9: ...oint provided 3 2 ACU I F This is designed to directly connect to the serial communications cable from an Advent SatFinder ACU4XXX or ACU5XXX control unit Detailed descriptions are beyond the scope of this manual Contact Advent Communications for further guidance and information Connector 15 pin female D type Pin Number Signal description 1 RS485 RX A 9 RS485 RX B 2 RS485 TX A 10 RS485 TX B 3 GND ...

Page 10: ...r further guidance and information Connector 25 pin male D type Pin Number Sensor Signal description 1 Sensor 1 12V DC supply 2 Signal input 14 GND 3 Sensor 2 12V DC supply 15 Signal input 16 GND 4 Sensor 3 12V DC supply 5 Signal input 17 GND 6 Sensor 4 12V DC supply 18 Signal input 19 GND 7 Sensor 5 12V DC supply 8 Signal input 20 GND 9 Sensor 6 12V DC supply 21 Signal input 22 GND 12 TX Position...

Page 11: ...e and information Connector 25 pin female D type Pin Number Sensor Signal description 1 Compass RS232 TX 2 RS232 RX 3 Compass 12V DC power 0 5A max 4 GND 5 GND 6 GPS GPS 12V DC power 0 5A max 7 RS232 TX 8 RS232 RX 9 GPS Enable 10 GND 14 Inclinometer Trigger 1 15 Trigger 2 16 Delta Pulse Width 17 Angle sign 18 Pulse width 1 19 12V DC supply 20 Pulse width 2 21 GND 22 GND 23 Waveguide Switch Drive p...

Page 12: ...ector PCB and an optional brake Detailed descriptions are beyond the scope of this manual Contact Advent Communications for further guidance and information Connector 15 pin male D type Pin Number Signal description 1 Motor phase A 2 Motor phase A 9 Motor phase A 10 Motor phase A 3 Motor phase B 4 Motor phase B 11 Motor phase B 12 Motor phase B 5 Brake active pull down 13 Brake supply 12V DC 6 MRD...

Page 13: ... F24 Stow sensor power supply alarm F25 MRD power supply alarm F26 Inclinometer power supply alarm F27 FPGA watchdog triggered F28 GPS comms failure F29 Compass comms failure F30 Feed drive failure F31 Handheld Controller override active F32 Alarm Error F33 Fin 1 over temperature F34 Fin 2 over temperature F35 Fin 3 over temperature F36 Fin 4 over temperature DCU4000 only F37 Fin 5 over temperatur...

Page 14: ...alarm and check the current fin temperatures Check that the side ventilation grills are clear to allow adequate airflow A short circuit of one of the stepper motor windings also causes the motor module to inhibit 4 5 F4 INCLINOMETER FAILED The inclinometer if fitted to the elevation axis has stopped responding to data requests The RF angle will be estimated using the systems internal elevation axi...

Page 15: ...n of the switch with the DCU on will trigger this alarm Switch is disconnected Switch is stuck or jammed 4 11 F10 AZIMUTH STOW SENSOR FAILED The sensor used to detect the azimuth tab markers has failed Possible causes Sensor disconnected Sensor failure Metal stuck in sensor 4 12 F11 ELEVATION STOW SENSOR FAILED The sensor used to detect the elevation tab markers has failed Possible causes Sensor d...

Page 16: ...r by more than 2 Action re calibrate axis The stow marker is not present The stow sensor or drive circuit has failed 4 21 F20 POL STOWING FAILED The system failed to detect the polarisation stow sensor in at its expected position Possible causes Excessive stall or freewheel has uncalibrated the axis so much the systems polarisation angle is in error by more than 2 Action re calibrate axis The stow...

Page 17: ... never be triggered if seen please report the occurrence to Advent Communications customer support 4 33 F33 FIN 1 OVER TEMPERATURE The measured temperature of heatsink fin 1 has exceeded 90 C The operating temperature of the unit is out of specification the unit side ventilation grills are blocked or the units cooling fan have failed 4 34 F34 FIN 2 OVER TEMPERATURE The measured temperature of heat...

Page 18: ...ot been detected on power up 4 46 F46 POL BRAKE DISCONNECTED The DCU5000 is expecting a brake to be fitted on the polarisation axis The brake has not been detected on power up 4 47 F47 AXIS 4 BRAKE DISCONECTED The DCU5000 does not have an axis 4 drive This alarm should never be triggered if seen please report the occurrence to Advent Communications customer support 4 48 F48 AXIS 5 BRAKE DISCONNECT...

Page 19: ...report the occurrence to Advent Communications customer support 4 56 F56 EXT FLASH ERROR An error has been detected erasing or writing to the DCU5000 flash memory chip 4 57 F58 HEATSINK FAN STALL DETECTED The heatsink fan on the motor drive output stage has been detected to be not turning This could result in the output stage overheating and shutting down to prevent thermal damage 4 58 F59 HMR3300...

Page 20: ...upplied must have the following parameters set RS485 interface 4 wire version Address 180 Baud rate 9600 8 data bits no parity 1 stop bit 5 3 PACKET STRUCTURE Advent uses a non printable packet format This means that the full range of 255 ASCII characters can appear in the message The format of all messages is STX BYTE COUNT ADDRESS DATA CHECKSUM ETX STX start of transmission STX is the ASCII char...

Page 21: ...mmand is an echo back of the command with associated parameters This indicates that the command has been accepted and the unit will attempt to action the command Note Receiving a response of this type does not mean that the command has been actioned Generally the action will occur after the response has been sent This is to ensure that all responses are returned quickly Average response time 300ms...

Page 22: ...is command Error 2 invalid parameters Responds with current settings Example Command to set the transmit gain to 50 0dB The command is GT and the valid range for the parameters is 000 to 400 Command sent GT500 Response from unit GT200 Result the response indicates that the parameters were not valid 50 0dB is outside the range for this unit Response indicates that the current value is 20 0dB i e no...

Page 23: ...ial number Query Software revision Command QSR Response Software Rev a aab bbc cc unit revision a aa antOS revision b bb antenna control revision c cc Query Software Part Number Command QSPN Response SPN Software Part No String Software Part No String ASCII software part number string max 30 characters Query FPGA revision Command QFR Response FRxx yy FPGA revision xx yy xx yy Number 00 99 Query lo...

Page 24: ... mu ut th h E E E El le ev va at ti io on n P P P Po ol la ar ri is sa at ti io on n x xx xx x M Mo ov ve em me en nt t i in n 0 0 0 01 1 u un ni it ts s Read Jog movement size Command RJM Response JM xxx R Re ea ad d a ac ct tu ua al l a an ng gl le e j jo og gg ge ed d f fr ro om m l la as st t j jo og g c co om mm ma an nd d x xx xx x A An ng gl le e m mo ov ve ed d U Un ni it ts s 0 0 0 01 1 R...

Page 25: ... H Response H Set Elevation Angle Command SEC xxx Response SEC xxx x xx xx x N Ne ew w E El le ev va at ti io on n a an ng gl le e i in n r ra an ng ge e 0 0 t to o 9 90 0 U Un ni it ts s 0 0 1 1 O On nl ly y w wo or rk ks s i if f s sy ys st te em m d de ep pl lo oy ye ed d e el le ev va at ti io on n a ax xi is s c ca al li ib br ra at te ed d a an nd d n no o i in nc cl li in no om me et te er ...

Page 26: ... Command QMT Response MT aaaa bbbb cccc dddd eeee ffff aaaa Internal ambient temperature Units 0 1 C bbbb Heatsink fin 1 temperature Units 0 1 C cccc Heatsink fin 2 temperature Units 0 1 C dddd Heatsink fin 3 temperature Units 0 1 C eeee Heatsink fin 4 temperature Units 0 1 C ffff Heatsink fin 5 temperature Units 0 1 C Fin not fitted Read DCU GPS Position Command RDGPS Response RDGPSabbbb bbbbcccc...

Page 27: ...The new compass offset takes about 1 second to update During this time the offset value is fixed at 800 0 Query Compass data Command RDCDT Response RDCDTW Data Field W Compass Type a Not fitted End of message b C100 type c HMR3300 C100 Data Field This is the only compass type currently XXXXXXX A B C100 YY MM DD D E F XXXXXXX Compass serial number A Software version B Hardware version C100 Compass ...

Page 28: ...Compass The calibration responses and final results are output using the QUD responses Abort calibration procedure Command WCSCA Response WCSCA Reset Pitch Angle HMR3300 only Command WCRPA Response WCRPA Sets the HMR3300 pitch angle to 0 Reset Roll Angle HMR3300 only Command WCRRA Response WCRRA Sets the HMR3300 roll angle to 0 ...

Page 29: ...bb ccccc ddddd eeeee fffff ggggg hhhh iiii jjjj kkkk llll mmmm nnn ooo rrr Coding aaaaa Azimuth ACW Tab Negative edge Units 0 01 bbbbb Azimuth ACW Tab Positive edge Units 0 01 ccccc Azimuth Stow Tab Negative edge Units 0 01 ddddd Azimuth Stow Tab Positive edge Units 0 01 eeeee Azimuth CW Tab Negative edge Units 0 01 fffff Azimuth CW Tab Positive edge Units 0 01 ggggg Polarisation ACW edge Units 0 ...

Page 30: ...s 0 1 s hhh Elevation max motor rate Units 0 1 s iii Polarisation max motor rate Units 0 1 s jj Azimuth motor current Units 0 1 A kk Elevation motor current Units 0 1 A ll Polarisation motor current Units 0 1 A m Azimuth motor fitted 0 Not fitted 1 Fitted n Elevation motor fitted 0 Not fitted 1 Fitted o Polarisation motor fitted 0 Not fitted 1 Fitted p Pol WGS fitted 0 No WGS fitted 1 WGS fitted q...

Page 31: ...e Units 0 1 s ooo Axis 5 max motor rate Units 0 1 s pp Azimuth motor current Units 0 1 A qq Elevation motor current Units 0 1 A rr Polarisation motor current Units 0 1 A ss Axis 4 motor current Units 0 1 A tt Axis 5 motor current Units 0 1 A u Azimuth motor fitted 0 Not fitted 1 Fitted v Elevation motor fitted w Polarisation motor fitted x Axis 4 motor fitted y Axis 5 motor fitted z Upper wooded a...

Page 32: ...ponse UA wwww xxxx yyyy zzzz wwww Azimuth angle Fixed length Units 0 1 xxxx RF Elevation angle Fixed length Units 0 1 Based on inclinometer readings yyyy Internal Elevation angle Fixed length Units 0 1 zzzz Polarization angle Fixed length Units 0 1 State Command QUS Response USABCBEFGH A System mode O Operational T Test U DUT B System Monitoring 1 On 0 Off C System State a STOWED b STOWING c DEPLO...

Page 33: ...bration Limit States Command QUL Response ULABCDE A Azimuth limits B Elevation limits C Polarisation limits D Axis 4 limits E Axis 5 limits Limit coding a OK b Clockwise softlimit c Anti Clockwise softlimit d Clockwise freewheel e Anti Clockwise freewheel f Clockwise travel limit g Anti Clockwise travel limit h Clockwise Stall I Anti Clockwise Stall Waveguide Switch Position Command QUW Response U...

Page 34: ...t 10 Azimuth stow sensor failure Bit 11 Elevation stow sensor failure Bit 12 Polarization stow sensor failure Bit 13 Stow 4 sensor failure Bit 14 Stow 5 sensor failure Bit 15 Stow 6 sensor failure Bit 16 MSB FPGA programming failure Alarm 2 Bit 1 LSB Manual brake override active Bit 2 Azimuth stowing failure Bit 3 Elevation stowing failure Bit 4 Polarization stowing failure Bit 5 Axis 4 stowing fa...

Page 35: ...ke disconnected Bit 14 Polarisation brake disconnected Bit 15 Axis 4 brake disconnected Bit 16 MSB Axis 5 brake disconnected Alarm 4 Bit 1 LSB Main unit fan over MTBF Bit 2 Heatsink fan over MTBF Bit 3 E2 PROM Checksum error Bit 4 Softlimit data error Reverted to defaults Bit 5 Wooded area data error Reverted to defaults Bit 6 Calibration area data error Reverted to defaults Bit 7 FPGA compatibili...

Page 36: ...reset Variable length Test Tab Measure Results Command Response TTR xxxxx yyyyy aaaaa bbbbb Returned after the successful completion of a force axis tab measurement in response to a QUD message xxxxx Edge 1 CW 1a Fixed length units 0 01 yyyyy Edge 2 CW 2a aaaaa Edge 3 ACW 2b bbbbb Edge 4 ACW 1b Compass calibration position request Command Response CCxxxx Requests vehicle to position x xxxx is vari...

Page 37: ...FITTED WITH AC DC POWER SUPPLY WARNING Hazardous voltages are present with lid removed Diagnostic work on AC powered units or PCBs must be carried out in a test area designated and equipped for live testing If units have recently been in operation time must be allowed for the discharge of capacitors before handling the unit 6 4 SATELLITE TRANSMISSION EQUIPMENT Radiation Hazard warnings should be p...

Page 38: ...k for any a typical heating of waveguide components using a Temperature Probe and Digital Volt Meter waveguide load will get hot during operation but interconnections should not C When transmitting through the antenna system check that spurious radiations at rear and sides of the antenna and outside the coned areas do not exceed currently accepted safe microwave radiated levels DO NOT PROCEED UNTI...

Page 39: ...rder for these services must be issued prior to field service 7 4 SHIPMENT OF REPAIR PARTS TO FIELD A purchase order for warranty repair parts must be issued prior to sending parts to field Parts will be priced at current prices and payment if full will be due if failed parts are not returned within 30 days regardless of responsibility of receipt of warranty parts If parts are shipped within the p...

Page 40: ...5 3HE England 7 7 AUTHORISATION FOR EVALUATION When any Product is returned for examination and inspection or for any other reason Customer and its shipping agency shall be responsible for all damage resulting from improper packing or handling and for loss in transit notwithstanding any defect or non conformity in the Product By returning a Product the owner grants Advent permission to open and in...

Page 41: ...Advent Communications 209297 DCU5000 Drive Control Unit Page 41 of 42 8 FIGURES ...

Page 42: ...Advent Communications FIGURE 1 DCU5000 LAYOUT 209297 DCU5000 Drive Control Unit Page 42 of 42 ...

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