Agenda:
Minutes:
Below is the plan I've come up so far for the database related part of the beam spot monitoring/control. The basic idea is as follows:
(1). The initial beam positions are used as a "static" parameter for each run. These parameters can be obtained from a special run such as a calibration run or some thing like that. Such a calibration might be needed for each new store of beam. The parameters should be stored in the online database and avaiable when a new run starts.
(2). The beam positions are constantly calculated by beam vertex EXAMINE during the data taking. Evert a few minutes(to be determined, depending on the statistics needed) the deviations relattive to the "static parameter are constantly monitored. Monitoring histograms or plots will be provided by EXAMINE for shifters and accelerator people.
(3). When the deviations exceed the threshold values, a special trigger is issued. This trigger activates the feedback to the accelerator control for the beam position adjustment; it also enables the entry of the new beam position information (after adjustment) into the database. This is the "dynamic" part.
I think if the above scheme works. The crucial question is how frequent the "dynamic" part is, and whether the "dynamic" info should be enetered in the same online database as the "static" parameters or some other database.
From the information I've collected and the understanding I've established so far, The occurrence of the "dynamic" trigger might not be high since the beam position fluctuation during the same beam store is expected to be well within +-100 microns. It is possible the trigger is issued every a few 10-minutes on average.
I should also point out that the above scheme is based on the assumption that the correction control is responsive. For example, a correction of 100 microns for beam control should take no more than a few minutes.
discussion:
Uli: what is the dynamic range of the correction dipoles?
answer: +- 1mm in position, +- 1.5 mrad in angle, provided that beam is on
nominal orbit and correction elements run at 0 A initially.