The PID controller for the velocity of the Altitude drive will
be included inside the LCU. It will provide an analogue signal as a reference
with +-10Vdc maximum to the current loop, which belongs to the supply of
the contractor and which may be included in his power amplifiers.
The tachometer shall provide an analog signal (+-10Vdc) proportional
to the actual speed of the drive system to the LCU as an analog symmetrical
signal via a screened twisted pair cable.
The connection between the encoder and the IK320 module in the
LCU is defined in [AD
07].
The limit switch and brake status shall be connected to
the ESO standard digital I/O board via the interlock system as defined in
the Electronic Design Specification [AD 01]. The interlock
system is supplied by ESO. The power 24VDC 0.6A for the PHASE drive is supplied
by the LCU.
The connection layout and pin assignment is given in [AN 01]Annex 1 VLT-DWG-ESO-15154-1769
|
|
|
|
|
|
|
|
||||
| PHASE Communication | RS485 Port - Protocol S-Link 3 [RD 06] | |||
|
Drive constant (amplifier+motor) Kt=92Nm/V |
||||
| 1 | LCU | ATS | Power On + Main power input relay |
24VDC, 100mA supply
to relay coil Digital output |
| 2 | LCU | ATS | Power On - | Common |
| 3 | LCU | ATS | Amplifier Enable | High = Enable
Contact closed to enable the amplifier output stage Toggling that signal resets externally triggered faults .e.i. PTC overtemperatures, Overspeed, encoder fail signal. Digital |
| 4 | LCU | ATS |
inhibit positive |
Low = inhibit is asserted when positive vicinity
limit is active. When the amplifier is in torque mode (nominal configuration) the ESO velocity speed loop sends apropriate command to stop further motion in the corresponding direction. |
| 5 | LCU |
ATS |
inhibit negative | Low = inhibit is asserted
when negative vicinity limit is active. When the amplifier is in speed mode(manual only), the Negative velocity reference is clipped; the amplifier stop further motion in the corresponding direction. When the amplifier is in torque mode (nominal configuration) the ESO velocity speed loop sends apropriate command to stop further motion in the corresponding direction |
| 6 | ATS | LCU | Overspeed | High = no overspeed.
The speed is sensed on the frequency of the Linear Hall Sensors, exceeding
the limit will set the Overspeed alarm and keep it latched until
the next enable cycle. Source Driver: 24V, 100mA max. Digital |
| 7 | ATS | LCU | DriveOK (no-fault)
|
High = DriveOK (no-fault). When negated (fault), the drive is disabled and latched
until a reset is applied. Detailed fault information via the serial
link. (Possible faults could be: tacho, hall sensor, over-under voltage,
over current,, 50 &70 over temperature etc…) Source Driver: 24V, 100mA max. Digital |
| 8 | ATS | LCU | 400VAC Power OK | High = the 400VAC Power
is OK. Source Driver: 24V, 100mA max. Digital |
| 9 | LCU | ATS | Amplifier drive power + | +24VDC, 1.2A |
| 10 | LCU | ATS | Amplifier drive power - | GND |
| 11 | unused | PE | ||
| 14 | LCU | ATS | Torque command + | Analog differential
+/-10V, Zin = 10kW Analog output |
| 15 | LCU | ATS | Torque command - | Analog differential
+/-10V, Zin = 10kW Analog output |
| 16 | Shield | PE | ||
| 18 | LCU | ATS | Speed /Torque mode |
High = Speed mode. |
| 19 | ATS | LCU | Motor Powered | High = 400V OK and Drive
enabled Source Driver: 24V, 100mA max. Digital |
|
scale = 11.72V*s/deg; speed = 1.7 deg/s at Tacho out = 20V Tacho output is positive when tube moves from horizon towards zenith |
||||
| 30 | ATS | LCU | Tacho signal + | Analog symmetric +/-10V,
5mA Analog input |
| 31 | ATS | LCU | Tacho signal - | Analog input |
| 33 | LCU | ATS | Tacho Range 8x | High = Sensitivity is
increased by factor 8. Contact status: 24VDC, 6.6kW to GND Digital |
| 34 | ATS | LCU | Tacho Range | High Sensitivity is
increased by factor 8. Source Driver: 24V, 100mA max. Digital, |
| 35 | ATS | LCU | Tacho OK | High = Tacho OK; the tacho signal
is ouput to ESO LCU. When Encoder OK is asserted, the drive amplifier uses the sine & cosine signals from the axis encoder for commutation and improved ripple performances. If coherency between the two signals is lost the tacho OK is negated. Source Driver: 24V, 100mA max. Digital, |
|
Heidenhain IK320 output : 1 V peak-to-peak, sine-cosine A,B signals |
||||
| 40 | LCU | ATS | A+ | Output A+ |
| 41 | LCU | ATS | A- | Output A- |
| 42 | Shield A | |||
| 43 | LCU | ATS | B+ | Output B+ |
| 44 | LCU | ATS | B- | Output B- |
| 45 | Shield B | |||
| 46 | Global Shield | Chassis GND | ||
| 47 | LCU | ATS | Encoder OK | High = Encoder OK and
available, The encoder is powered and provides the sincos incremental signals. The drive amplifier performs a coherency check between the sine and cosine signals. 24VDC,Source Driver: 24V, 100mA max. Digital, |
|
|
||||
| 50 | ATS | LCU | Vicinity PLS + | Contact opens if positive
vicinity limit is crossed Digital |
| 51 | ATS | LCU | Vicinity PLS - | Common |
| 52 | Shield | PE | ||
| 53 | ATS | LCU | Vicinity NLS + | Contact opens if negative
vicinity limit is crossed Digital |
| 54 | ATS | LCU | Vicinity NLS - | Common |
| 55 | Shield | PE | ||
| 56 | ATS | LCU | Interlock PLS + (Positive Limit+) | Contact opens if positive
interlock limit is crossed Digital |
| 57 | ATS | LCU | Interlock PLS - (Positive Limit-) | Common |
| 58 | Shield | PE | ||
| 59 | ATS | LCU | Interlock NLS + (Negative Limit+) | Contact opens if negative
interlock limit is crossed Digital |
| 60 | ATS | LCU | Interlock NLS - (Negative Limit-) | Common |
| 61 | Shield | PE | ||
| 62 | ATS | LCU | Altitude Locking pinA + | 10 to 30 VDC |
| 63 | ATS | LCU | Altitude Locking pinA - | Common |
| 64 | ATS | LCU | Altitude Locking pinA signal | High = Altitude Locking
pin is disengaged. Open collector PNP, 200 mA max. Digital |
| 65 | ATS | LCU | Altitude Home switch + | 24V logic Transition
at about 5 degree Zenithal distance; open at Zenith, closed at Horizont |
| 66 | ATS | LCU | Altitude Home switch - | Common |
| 67 | Shield | |||
| 68 | ATS | LCU | Altitude Locking pinB + | 10 to 30 VDC |
| 69 | ATS | LCU | Altitude Locking pinB - | Common |
| 70 | ATS | LCU | Altitude Locking pinB signal | High = Altitude Locking
pin is disengaged. Open collector PNP, 200 mA max. Digital |
| 71 | ATS | LCU | EndStopA + | On Nasmyth A side a Zenith or a Parking End Stop schock absorber is not in position Contact opens |
| 72 | ATS | LCU | EndStopA - | Common |
| 73 | ATS | LCU | EndStopB + | On Nasmyth A side a Zenith or a Parking End Stop schock absorber is not in position Contact opens |
| 74 | ATS | LCU | EndStopB - | Common |
| 80 | ATS | LCU | Motion Stop + | 24VDC, 8W max. |
| 81 | ATS | LCU | Motion Stop - | Common |
| 82 | Shield | |||
| 83 | ATS | LCU | Transporter relocation+ | High = Transporter in
station position. Low = Altitude immobilized because AT not in station position. See IfTransporter_RelocationStatus 1 Digital line, pulled down to GND |
| 84 | ATS | LCU | Transporter relocation- | |
| 85 | Shield | |||
|
|
||||
| 90 | ATS | LCU | Status B side + | 8 NO switches in serie,
30 VDC, 10A max. Contact closed when brakes are disengaged Digital input |
| 91 | ATS | LCU | Status B side - | 8 NO switches in serie,
30 VDC, 10A max. Contact closed when brakes are disengaged Digital input |
| 92 | ATS | LCU | Status A side + | 8 NO switches in serie,
30 VDC, 10A max. Contact closed when brakes are disengaged Digital input |
| 93 | ATS | LCU | Status A side - | 8 NO switches in serie,
30 VDC, 10A max. Contact closed when brakes are disengaged Digital input |
| 94 | LCU | ATS | Brake command | High = Enable
Contact closes to disengage the brakes |
| 95 | LCU | ATS | Return | Common |
|
|
||||
| 100 101 |
ATS | LCU | Signal monitoring | Buffer amplifier output
+/- 10V ,5mA differential for monitoring of internal amplifier variable
selected via the serial communication link. Relevant signals for monitoring:
|
| 110 | LCU | ATS | Signal selection | Saturation parameters:
|
|
|
|||||
| E
S O o n l y |
Item | From | To | Signal | Description |
| 1 | ATS | LCU | Motion Stop + | 24VDC, 8W max. | |
| 2 | ATS | LCU | Motion Stop - | Common | |
| 3 | ATS | LCU | Relocation + | High
= Transporter in station position. Low = Altitude immobilized because AT not in station position. |
|
| 4 | ATS | LCU | Relocation - | ||
| 5-23 | SPARE | SPARE | |||
| 24 | LCU | LCU | PHASE R/TX+ | PHASE RS485 communication link | |
| 25 | LCU | LCU | PHASE R/TX- | ||
| 26 | LCU | LCU | PHASE return R/TX+ | ||
| 27 | LCU | LCU | PHASE return R/TX- | ||
| 28 | Ground | ||||
| 29 | Ground | PMAC RS232 communication link | |||
| 30 | LCU | LCU | PMAC TxD | ||
| 31 | LCU | LCU | PMAC RxD- | ||
| 32 | LCU | LCU | PMAC RTS | ||
| 33 | LCU | LCU | PMAC CTS | ||
| 34 | LCU | LCU | Ground | ||
| 35 | LCU | LCU | PMAC return TxD | ||
| 36 | LCU | LCU | PMAC return RxD | ||
| 37 | LCU | LCU | PMAC return RTS | ||
| 38 | LCU | LCU | PMAC return CTS | ||
| 39 | LCU | LCU | CPU0 RXD | RS232 communication link | |
| 40 | LCU | LCU | CPU0 TXD | ||
| 41 | LCU | LCU | Ground | ||
| 42 | LCU | LCU | Ground | ||
| 43 | LCU | LCU | CPU1 TXD | RS232 communication link | |
| 44 | LCU | LCU | CPU1 RXD | ||
| 45-48 | SPARE | ||||
Last modified: Mon Jan 20 10:59:26 MET 2003