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Mnemonic:

SWI_2D_MAP_FS_V1

Name:

SWI 2D MAP FS V1

Description:

Same as SWI 2D MAP PS, except a frequency-switch calibration mode is
used instead of position-switch. It enables spending 100% of the integration time on-source. If
the purity of the spectral band is good enough, there is an option to pre-compute ON-OFF for
the CTS before downlink.

Payload:

SWI

Pointing

Pointing Type:

nadir

Target:

PTRSnippet file:

Advanced

Scheduling Rules:

Scheduling: d1–d3 for pointing calibration and global maps,
d1/d2 for meridional scan, d1 for zonal scan. Repetition: depends on science goal priorities.
Moon monitoring: when Galilean moons are well-resolved (angular diameter >2mrad). Flyby:
This mode will be continuously used during phase IV, and phases I and III of the flybys between
12hrs and 6hrs from CA. GCO-500: this mode will be used in configuration (1) continuously
for 5 orbits (i.e. 16-hrs) and then cycled equally with SWI MOON LIMB SCAN FS,
SWI MOON LIMB STARE FS, and SWI MOON NADIR STARE FS. Scheduling and repetition
of configuration (2) depends on science goal priorities.

any rule that is used to schedule the observation: repetition rules, continuous (plasma instruments), one-off, every orbit, every day, etc

Avoidance Rules:

TBD

conditions that make the observation not possible (e.g. thruster firing)

Comments:

Support Plot 1:

Support Plot 2:

Support Plot 3:

Commanding

ITLSnippet file:

Related segment definitions

	Segmentdefinition
Segment	E_GPH_OBS
Segment	E_RS_OBS
Segment	E_RS
Segment	E_RS_6E1
Segment	E_RS_7E2
Segment	E_RS_7E1
Segment	E_RS_8E2
Segment	E_GPH
Segment	E_GPH_6E1
Segment	E_GPH_7E2
Segment	E_GPH_7E1
Segment	E_GPH_8E2

Power profiles

	Event	Time	Mode	User Defined Power (Watts)	Comment
Start 00:00:00 User Defined 67.43 [Watt]	Start	00:00:00	User Defined	67.43	basic long peak power

Data profiles

	Event	Time	Mode	User Defined Data Rate (bit/s)	Comment
Start 00:00:00 User Defined 5733.0 [bit/s]	Start	00:00:00	User Defined	5733.0	Maximum data rate: 5.733kbit/s (Jupiter), 0.512kbit/s (Moon monitoring), 0.624kbit/s (Flyby), 0.816kbit/s (GCO(1)), 3.173kbit/s (GCO (2)) Minimum data rate: 0.483kbit/s (Jupiter), 0.402kbit/s (Moon monitoring), 0.404kbit/s (Flyby), 0.407kbit/s (GCO (1)), 0.443kbit/s (GCO (2))

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