SbandObservingInfo
Back to current versionRestore this version

Observing with EIS with the new antenna#

Table of Contents

#

About this page#

This Wiki page deals with typical observing constraints that you need to bear in mind when making a proposal for observing with Hinode EIS.

Practical constraints#

Time#

OP Periods#

An OP Period[1] is the period of time during which an observing programme (plan) is defined. e.g. from 10:23 UT on 2008/05/02 to 11:19 UT on 2008/05/04. (The start and end of each OP period are determined by the pattern of ground-station contacts, which varies from day to day.)

Since the transition to stable operations under the S-band antenna, typical OP Period durations have been two or three days.

Once solar activity begins to increase, and solar unpredictability increases accordingly, Hinode may consider more frequent (i.e., one-day-long) OP Periods.

Post-pointing delay#

In order to have co-ordinated observations by its three instruments, Hinode points as a whole satellite (using its AOCS[6]), either tracking a point to compensate for the (differential) rotation of the Sun, or focusing on a fixed point. Either way, changes in pointing by the s/c[7] take time to stabilise. After approximately 90 seconds, Hinode can track or fix on a point with better than 1" accuracy, below the spatial resolution of EIS and XRT.

To avoid observing during the stabilisation of pointing, EIS observations normally start at least two minutes after a satellite re-point.

To see what an Hinode re-pointing schedule looks like, take a look at an example on the Hinode Daily Operations website here

Eclipse Season#

During eclipse season[5], the line of sight between the spacecraft and the Sun grazes the Earth's atmosphere, causing attenuation (and ultimately complete absorption) of the light that would otherwise be seen by each of the instruments. This attenuation affects first the EUV and X-ray bands, then later the visible wavelength range.

The duration of night-time is calculated for the visible band, and in the peak of eclipse season (around mid-July [3]) this duration is about 20 minutes. EUV absorption (night ingress) begins about 10 minutes before the calculated entry into optical night (listed as NGT_ENTRY) and ends (night egress) in the EUV about 10 minutes after the optical band exit (NGT_EXIT). Thus, the EIS operations team recommend that you leave a ten-minute buffer around s/c night in eclipse season where possible. Extended-duration observations

At the middle of eclipse season, clear EUV day (i.e., not including transition into or out of eclipse) lasts for approximately 60 minutes (not taking into account expansion of the ionosphere with increased solar activity). So it's a good idea to limit your study to this duration if you intend it to be able to run during eclipse season.

South Atlantic Anomaly (SAA)#

On most orbits[8], Hinode passes over the South Atlantic Anomaly (SAA), where high-energy particles penetrate lower into the magnetosphere. During such passes, significantly more cosmic rays are observed on the EIS detector images. These passes are calculated at the same time as other orbital events (such as Eclipse Season NGT events, when appropriate), and times vary each day. Such passes normally last approximately 10 to 20 minutes (although they can be calculated to last for as little as 30 seconds).

However, around 12 UT, Hinode experiences a so-called Golden Period where the SAA itself does not intercept the s/c orbit. Because the SAA passes vary in time, the start of this period can range (approximately) from 10 to 11 UT, with the end being anywhere from 14 to 16 UT.

The EIS team use a rule of thumb that a 5-minute window around SAA events is sufficient to account for the variability in size of the anomaly itself.

N.B. the old vulnerability to changing slit/slot choice during an SAA pass is no longer relevant, following an on-board software update in August 2007

Buffer summary#

The table below summarises the time buffers recommended to separate observations from the corresponding events.

Event Buffer
Re-point 2 minutes after
SAA_ENTRY 5 minutes before
SAA_EXIT 5 minutes after
NGT_ENTRY 10 minutes before
NGT_EXIT 10 minutes after

Volume#

Typical volume allocation#

Since moving to Hinode's S-band antenna for downlinks, the spacecraft typically can downlink something like 200 Mb[2] per 24 hours. This is worked out by the total contact time at all ground-stations, multiplied by the bandwidth to the ground.

Do you have examples of what kind of observations are best suited for EIS?#

Yes :-)

Go over to the Study4LowDataVolume page on this Wiki for examples of programmes recently developed for EIS.

Why can my old HOP no longer be run?#

How is the HOP process different?#

Nomenclature#

OP
[1]Operation Programme
S-band antenna
[4] Hinode's secondary antenna, with a bandwidth of 262 kb/s.
Eclipse Season
[5] The portion of the year where the sun is occluded by the Earth's atmosphere for a fraction of each orbit. It lasts from late April until early September.
AOCS
[6] Attitude and Orbit Control System
s/c
[7] abbreviation of spacecraft
Other Notes

[2]: Remember, Mb stands for megabits (1024 × 1024 bits), as distinct from MB (for megabytes). 1 MB = 8Mb.

[3]: Is this correct? I know it's approximately true, since we start in late April, and come out of eclipse season in early September.

[]: Hinode's orbital period is 98.5 minutes

put your CopyrightNotice in here !