Gap analyses by variable, type of mission or WIGOS subcomponent Help icon

Select gap analysis type

Select analysis type

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In "Simplified" mode, the results in the analysis are calculated by looking at each instrument's mission objectives: for each instrument we keep track of what the primary, secondary, and opportunity mission objectives are. These mission objectives indicate that an instrument is primarily envisioned to measure variable X, Y and Z, that variables A, B and C are its secondary objective, and that it may offer the opportunity to measure variables I and II although it is not optimized for that. The simplified Gap analysis produces a timeline based on this information. The simplified Gap analysis is only available for analyzing variables, not for missions.
In "Expert system" mode, the results in the analysis are calculated with an expert system. Internally, OSCAR works with a large set of 1700 rules that determine whether or not an instrument is capable of measuring a given variable, and to what degree. When you select "Expert system", the Gap analysis is performed based on this large set of rules.

Select a Variable

Select a type of Mission

Select a WIGOS subcomponent

Variable sorting criteria

 

Each instrument is assigned with an up-to-5-step rating, evaluated as a blend of several elements.  For this particular Variable, the rating is driven by:

  • the observed solar area (disk only or disk + corona);
  • the spatial resolution at solar surface
  • whether measuring flux or spectrum.

 

RATING CRITERIA:

1

  • Disk only, high spatial resolution spectrometer, polarimetric and Doppler capability
  • Disk + corona, high spatial resolution fluxmeter, polarimeteric and possibly Doppler capability
  • Disk only, high spatial resolution fluxmeter, polarimeteric and possibly Doppler capability

2

  • Disk only, coarse spatial resolution spectrometer, polarimetric and Doppler capability
  • Disk + corona, coarse spatial resolution fluxmeter, polarimeteric and possibly Doppler capability
  • Disk only, coarse spatial resolution fluxmeter, polarimeteric and possibly Doppler capability

3

  • Disk + corona, high spatial resolution spectrometer or fluxmeter
  • Disk only, high spatial resolution spectrometer or fluxmeter

4

  • Disk + corona, coarse spatial resolution spectrometer or fluxmeter
  • Disk only, coarse spatial resolution spectrometer or fluxmeter

5

  • -
Measurement timeline for Solar VIS image Help icon
Hint: Move around in the timeline by scrolling up, down, left or right.

Found 13 results

This table has a large number of results.
Instrument NRT? Relevance Satellite ECT/Lon Orbit DLR
1992
1993
1994
1995
1996
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1998
1999
2000
2001
2002
2003
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2006
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2015
2016
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2018
2019
2020
2021
2022
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2025
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2033
2034
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2036
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2039
2040
2041
MDI Important note1 - primarySOHOL1
X
XXXXXXXXXXXXXXXXXXXXXXXXXXXXXX
PHI1 - primarySolar Orbiter25 °Solar
X
XXXXXXXXXX
PMI1 - primaryVigil-L5L4-L5XXXXXXXXXXX
SOT Important note1 - primarySolar-B (Hinode)06:00 ascSunSync
X
XXXXXXXXXXXXXXXXXX
HMIYes1 - primarySDO29.6 °GeoSync20
X
XXXXXXXXXXXXXX
SoloHI3 - highSolar Orbiter25 °Solar
X
XXXXXXXXXX
STEK3 - highZond-MTBDSunSync
X
XXX
WISPR3 - highParker Solar Probe3.4 °Solar
X
XXXXXXX
XRT3 - highSolar-B (Hinode)06:00 ascSunSync
X
XXXXXXXXXXXXXXXXXX
AIAYes3 - highSDO29.6 °GeoSync20
X
XXXXXXXXXXXXXX
SODISM3 - highPicard06:00 ascSunSync
X
XXX
X
TEREK-C4 - fairCoronas-I82.5 °DRIFT
X
TEREK-C4 - fairCoronas-F82.5 °DRIFT
X
XXX
X
All instruments for measuring Solar VIS image
Instruments Relevance Operational limitations
MDI1 - primary
PHI1 - primary
PMI1 - primary
SOT1 - primary
HMI1 - primary
SoloHI3 - high
STEK3 - high
WISPR3 - high
XRT3 - high
AIA3 - high
SODISM3 - high
TEREK-C4 - fair