70µm NF Focal Plane Survey, Coarse

Principal: Jocelyn Keene
Deputy: Jane Morrison, Bill Wheaton
Data Monkey(s): Jane Morrison and Bill Wheaton
Priority: Critical
Downlink Priority: Normal
Analysis Time: Campaign I: 2880 minutes, Campaign J: 2880 minutes, combining results from I and J: 120 minutes.
Last Updated:


Objective

To measure the pixel locations (i.e. array orientation, scale,and distortion) as a function of scan mirror angle for the 70 µm narrow field array configuration.

Description

Use an IER based on 70 µm Super-Resolution photometry AOT for to measure the locations on the sky of several positions on the array as a function of scanning mirror angle.
This task is run in campaigns I and J. The data from each campaign is processed separately by the MIPS and IPF teams. The IPF team then combines the results from both campaigns. The results from the IPF multi-run are used to update Frame Table 12. The results from campaign I are used to for FTU 10. The frame table updates for all the campaigns can be found in the following table:
Frame Table Updates.

Data Collected

The observing straiter is similar to the 70 µm Wide coarse survey. Except more observations are done resulting in 762 observations. The extra observations result from repeating the basic 11 observations at 6 locations on the array 11 times, instead of 7 times as in the 70 µm wide survey.

Calibration Star

For the selected calibration star see the IER for this survey. The requirements on the 70 µm coarse focal plane calibration star are as follows:

  • In CVZ
  • Mips requirements: stellar brightness corresponding to S/N of 30 (3 sec integrations) 0.094 Jy, K mag 2.14

    Observing Strategy


    Figure 1. Observing Pattern at 3 locations on the detector. Note size of box is not the total size of the array but a portion of the central region which depends on array and if it is a coarse or fine survey

    Definitions:

  • W axis direction is defined by the Frame Table, and is always within +/- 90 degrees of the TPF z axis as projected on the sky. Motion along this axis corresponds to motion in the spacecraft motion (left/right).
  • V axis direction is defined by the Frame Table, and is always within +/- 90 degrees of the TPF y axis as projected on the sky. Motion along this axis correspond to motion in the scan mirror direction (up/down).
  • W offset, the amount of motion in the W direction which results in the spacing between left array, middle array and right array observations
  • V offset, the amount of motion in the V direction which occurs between a set of observations.

    70 µm Coarse FPS observational parameters:

  • W offset = 50 arc seconds
  • V offset = 25 arc seconds
  • W dither = 7.5 arc seconds
  • V dither = 7.5 arc seconds
  • mirror locations for 1 position shown in figure 1.
    1. position 1 = 0
    2. position 2 = -75
    3. position 3 = 25
    4. position 4 = -50
    5. position 5 = 50
    6. position 6 = -25
    7. position 7 = 75
    8. position 8 = position 1 = 0

    Observational Strategy

  • Step 1
    1. PCRS observation
  • Step 2 - (total of 11 observations)
    1. Position the telescope so the data falls on the left side of array
    2. Position star at position 1 in figure 1 (left), turn stim on take an observation
    3. Turn stim off
    4. Take 8 DCES at positions shown in figure 1 (left)
    5. Position star at position 1, turn stim on and take observation
    6. With star still at position 1 turn stim off and take observation
    7. dither in V and W
    8. Repeat above 11 observations.
  • Step 3
    1. Move the space craft according to the W offset (50 arc seconds), image should now be on the center of the array.
    2. Position star at position 1 in figure 1 (middle), turn stim on take an observation
    3. Turn stim off
    4. Take 8 DCES at positions shown in figure 1 (middle)
    5. Position star at position 1, turn stim on and take observation
    6. With star still at position 1 turn stim off and take observation
    7. dither in V and W
    8. Repeat above 11 observations.
  • Step 4
    1. Move the space craft according to the W offset (50 arc seconds), image should now be on the right side of the array.
    2. Position star at position 1 in figure 1 (right), turn stim on take an observation
    3. Turn stim off
    4. Take 8 DCES at positions shown in figure 1 (right)
    5. Position star at position 1, turn stim on and take observation
    6. With star still at position 1 turn stim off and take observation
    7. dither in V and W
    8. Repeat above 11 observations in step.
  • Step 5
    1. PCRS observation
  • Step 6: move telescope according to V offset (25 arc seconds) and repeat steps 1-5
  • Step 7: move telescope according to V offset (25 arc seconds) and repeat steps 1-5
  • Step 8: move telescope according to V offset (25 arc seconds) and repeat steps 1-5
  • Step 8: move telescope according to V offset (25 arc seconds) and repeat steps 1-5
  • Step 9: move telescope according to V offset (25 arc seconds) and repeat steps 1-5
  • Step 10: move telescope according to V offset (25 arc seconds) and repeat steps 1-5
  • Step 11: move telescope according to V offset (25 arc seconds) and repeat steps 1-5
  • Step 12: move telescope according to V offset (25 arc seconds) and repeat steps 1-5
  • Step 13: move telescope according to V offset (25 arc seconds) and repeat steps 1-5
  • Step 14: move telescope according to V offset (25 arc seconds) and repeat steps 1-5

    Number of observations from step 1-5, 66. Step 1-5 repeated 7 times for a total of (66 * 11) = 726 observations.

    
    

    Data Reformatting Requirements

    Array Data Desired:

    70 µm NF

    Data Reformatting Option:


    Task Dependencies

    The telescope must be focussed.
    The S/C must be pointing and tracking optimally.
    The PCS, PCRS, and IRU must be calibrated.
    The 70 um array and scan mirror must be fully operational.
    The 70 um photometry AOT must be validated.

    Calibration Dependencies


    Output and Deliverable Products


    Data Analysis


    Software Requirements


    Actions Following Analysis


    Failure Modes and Responses


    Additional Notes