Telecon 20180214
Attending: Brian, Amy, Roger, Al, Kris, Julian, Jacques, Karl, Qi
Notes by : Qi
Agenda
2.5 day Workshop: May 1,2,3; in Minneapolis.
Telescope and instrument I+T (Tomo, Bill J)
Telescope I+T
(Tomo)
Receiver, Bill Jones
Attitude control requirements (Jacques)
Images from Kris
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Focal Plane updates (Karl)
Focal plane slides
Notes
Workshop
Working on program, plan to release in next few days
about: science, report, white paper if there is, data complement other data sets
Spacecraft (Amy)
we will need space craft bus, everything around the instrument
biggest challenge is point the instrument, spinning ,precession
mission TeamX
orbit (shape, size of orbit, sun & moon), ground processing
industry parter, preliminary design;
requirement for the craft, pointing stability & accuracy, mass, power we need
a week after TeamX
Attitude control requirements (Jacques)
sampling requirement
For CORE, 1/4th, constrained by scan strategy
for each position on the sky, we want to compare compare data, important for systematics
The requirement of sampling will translate to the requirement of altitude
Uncertainty on the position of spin axis, from one scan to other, translated to difference between two scans.
good control helps reduce gaps as much as we can
Cross-scan sampling per precession
Currently, T_prec = 10 hours, T_spin = 1 min, which lead to theta = 3'
3' is good for 100
GHz
, but not above; we can change T_spin or T_precession
Kris does not think changing T_precession / T_ spin can solve the problem globally. Very long precession, penalty is pile up enormously at poles.
we are assuming engineering achieving nominal, by 1 arcmin in 3 sigma error per spin.
Point reconstruction
alignment of instrument FOV with reference of spacecraft. change should not be faster than calibration
Jacques: we need to do simulation to get final number for point reconstruction
Shaul: 1’’ will be driven by systematics. We will see if 1’’ is reasonable given r value.
Amy: too loose, worse systematics; too tight, expensive to engineering.