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Figure of Merit for Infrared Sky Survey - FOM Approach

This presentation discusses the potential terms and concerns related to the Figure of Merit (FOM) for an Infrared Sky Survey. It explores the capabilities versus the implementation plan, suggesting a preferred solution based on satellite capabilities. The presentation presents a proposed general form of the FOM and addresses concerns regarding telescope diameter, field of view, pixel scale, and survey strategies. It also discusses the number of imaging and spectroscopic modes and the importance of mission lifetime. Additionally, it proposes an alternative implementation-based FOM.

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Figure of Merit for Infrared Sky Survey - FOM Approach

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  1. Figure of Merit (FOM) for Infrared Sky Survey Daniel Stern (JPL/Caltech) WFIRST Meeting 2011 March 11

  2. Approach • Brainstorm potential terms in FOM. • Raise some concerns: many addressed, but not all. This will be a job for the Survey Science Working Group. • Suggest a potential FOM at the end, but obviously should not be considered final.

  3. Capabilities vs. Implementation Plan • Should FOM be based on telescope design, or should it be based on a planned survey(s)? • Former addresses telescope capabilities, but doesn’t address implementation (e.g., survey plan doing only a single image per sky position is not as good vis-a-vis systematics as one doing 3+ images per sky position) • Latter doesn’t address guest observer (GO) capabilities, but could easily relate a FOM to the etendue (area x depth) of surveys. • My preferred solution: go with satellite capabilities to define FOM.

  4. General Form of FOM FOM ~ D2 × FOV × Nmodes × T • Essentially defines the FOM as the etendue of the telescope (collecting area times field of view) times the number of observing modes times the mission lifetime • Next slides will discuss concerns with each of these terms.

  5. Telescope Diameter • Simply using the telescope diameter doesn’t address optical design (e.g., TMA vs. off-axis anistigmic), mirror throughput (which could be wavelength dependent), etc... • Rather than scaling by D2, scale by the effective diameter, Deff2.

  6. Field of View (FOV) • Simply using the telescope FOV doesn’t address pixellation. Want to have some sort of weighting to FOM that pushes design towards the diffraction limited imaging. • Add a fudge factor to FOV, such as • f(FOV) = 1, if x≤1 • f(FOV) = 1 - κ(x-1)2/x2, if 1≤x≤XX • f(FOV) = 0, if x≥XX • where x = (pixel scale / diffraction limit)

  7. Field of View (FOV) or should this be at x=10? asymptote to zero?

  8. Field of View (FOV) • Simply using the pixel scale as the resolution doesn’t address survey strategies which could “buy back” diffraction limited imaging through post-processing (“drizzling”). • Should also give extra weight to resolutions that are not accessible from the ground. • Use the effective resolution, e.g., for a mosaicked wide-area shallow survey comprised of 4 drizzled images per sky position.

  9. A Few Related Concerns • I’m still concerned about not penalizing observing plans that are insufficiently redundant. Really want 3+ images per sky position to be able to control for systematics (e.g., bad pixels, cosmic rays, scattered light, etc...). But this is perhaps a secondary point if we base the FOM on satellite capabilities rather than survey implementation design. • Relatedly, I’m concerned about surveys that would hit the confusion limit; e.g., depth of survey is more relevant than collecting area. However, this is perhaps a pedantic point for the ensemble of likely WFIRST designs. • Were FOM to be designed for survey strategies, Ned suggested weighting by coverage: • coverage ≥ 4 : weight = 1 • coverage = 3 : weight = 0.5 • coverage = 2 : weight = 0.25 • coverage = 1 : weight = 0.125

  10. N (im.): Number of Imaging Modes • Want to reward more flexible missions, e.g., those with multiple filters. • Concern #1: Filter throughput / sensitivity should be included as a weighting factor. Implies making FOM ~ Σ(weighted imaging modes) rather than multiplying by number of imaging modes. • Concern #2: If weighting by sensitivity, need to worry about confusion noise and whether or not observations are background limited. However, these depend on survey implementation. • Concern #3: Should give extra weight to space-unique capabilities. E.g., weight imaging mode by sqrt(background from the ground / background from space). This would make 3 micron channel ~40x more compelling than 2 micron channel, and ~100x more compelling than 1 micron channel.

  11. N (sp.): Number of Spectroscopic Modes • Concern #1: How to combine imaging and spectroscopy / how to do the relative weighting. • Concern #2: FOM presumably scales with wavelength coverage. • Concern #3: How to weight spectral resolution, R?

  12. T: mission lifetime • longer mission is obviously better. • if multiple modes can be exercised simultaneously, then this is obviously a related boost. • ergo, multiple (focused) missions are also beneficial.

  13. Suggested Form of FOM Σ FOM ~ T × Deff2 × FOV × fmode • sum over observing modes, with a fudge factor fmode to account for: • system throughput • resolution relative to diffraction limit • background level relative to ground-based observations • spectral resolution • also need to scale by number of modes that can be done simultaneously

  14. Implementation-Based FOM • E.g., if FOM were to be based on survey implementation instead of satellite capabilities, then an alternative form of the FOM might be: FOM ~ area × depth × Nmodes

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