Next: FOFB Status
Up: ORBIT CONTROL AT THE
Previous: SOFB Results
In contrast to the SOFB, which runs on a central PC,
the global FOFB is decentralized and integrated in the
twelve BPM stations of the SLS storage ring. The feedback will operate
with an update rate of 4 kHz. Each of the twelve stations handles six
BPM inputs and six corrector magnet outputs. The design of the FOFB
at an early stage in the SLS project made it possible
to combine the feedback with the digital BPM system without much
additional expenditure. The hardware implementation of one of the
twelve BPM stations is shown in Fig. 5. The six BPM
position readings (
,
) of the sector are already available in a
digital format on a first digital signal processor (DSP 1). They are
transfered over a multiprocessor bus to a second processor (DSP 2)
which is devoted to the orbit feedback. Since the coefficients of the
inverted response matrix only have significant values around the
diagonal it is sufficient to calculate the new corrector magnet
settings with the adjacent BPM readings [7]. The
required beam positions from the neighboring sectors are exchanged
over a dedicated fibre optic point-to-point network. It uses the SHARC
link ports to which a fibre optic module is attached. Separate
channels for transmit and receive have been chosen between each sector
thus avoiding any network collisions. The whole processing chain is
driven by the data acquisition of the digital BPM system which in turn
receives hardware triggers from the timing system. An interrupt is
generated on DSP 1 as soon as data arrives from the digital
receivers. After transferring the position readings to DSP 2 an
interrupt is triggered to start the data exchange over the fibre links
with four parallel DMA processors. Data packets of 56 Bytes are
transmitted containing additional start and stop bytes. A timer
monitors whether the adjacent sectors have responded within a
predefined time window. Measurements in the laboratory between two VME
crates have shown that the full data exchange requires in the order of
8
s. Once the full set of BPM data of three sectors is available
the predefined reference orbit is subtracted resulting in the final
beam displacement. The sub-matrix multiplication yields the
incremental corrector magnet changes which are then written over the
VME bus to the power supply controller interface board. The VME bus
master capability of the DSP board avoids any necessary intervention
of the control system IOC. From the interface boards the new corrector
settings are transfered star like to six digital power supply
controllers over fibre optic links operating at 5 Mbits/s.
Next: FOFB Status
Up: ORBIT CONTROL AT THE
Previous: SOFB Results
Michael Boege
2002-06-19