Enclosure 4 - L10 Geometric Error Budget (GEB).pdf

Approval Date in

TDMS

Date

Approval Date in

TDMS

DateCagatay Aymergen

Landsat Next Geometric Error Budget Signature/Approval Page

Prepared by:

Electronic Signature in TDMS Angela Russo Landsat 10 Mission System Engineer NASA/GSFC, Code 533

Approved by:

Electronic Signature in TDMS

Landsat 10 Deputy Project Manager Acting CCB Chair NASA/GSFC, Code 426

CM FOREWORD

This document is a Landsat 10 Project Configuration Management (CM)-controlled document.

Note: Prior to February 2026, the project name was Landsat Next (LNext).

For the purposes of configuration management, the prefixes “LNEXT” and “L10” are completely interchangeable. For example, LNEXT-MGMT-PLAN-0004 is the same as L10-MGMT-PLAN- 0004.

Changes to this document require prior approval of the applicable Configuration Control Board (CCB) Chairperson or designee. Proposed changes shall be submitted to the Landsat 10 CM Office (CMO), along with supportive material justifying the proposed change. Changes to this document will be made by complete revision.

Questions or comments concerning this document should be addressed to:

NASA/Goddard Space Flight Center Landsat 10 Project Office, Code 426 Attention: Configuration Management Office Greenbelt, Maryland 20771

Revision Change Request Number Description of Change Release Date

- LNEXT-CCR-0017 Initial Release 12/05/22 A LNEXT-CCR-0056 Tables and error trees in the GEB budget/allocation excel file, and associated PPT companion file were updated to reflect “relative knowledge” terminology and to define the orbit period as a “98-minute” time span. This content was discussed, vetted, and finalized during the 3/1/2023 Pointing Jitter Alignment Working Group Meeting.

04/26/23

B L10-CCR-0140 Change document number from LNEXT-SYS-DESC-007 to L10- SYS-DESC-007. Update project name from Landsat Next (LNext) to Landsat 10 (L10). Update SRD requirement numbers from LN-SRD-XXX to SRD-XXX.

03/25/26

CHANGE HISTORY LOG

Pointing 3-sigma

Allocation Units Scale to Ground Units LE90 CE90 Source

L9 MCDR

Estimate

L9 On-Orbit Estimate Owner

L9 Heritage Requirement

LNext Requirement Source/Rationale End-to-End Geometric Performance L10 Level-3

L10 Requirement

Abs.

Geodetic

LaRD-1078 Geometric LaRD-1082

VSWIR

B2B

LaRD-1073

VSWIR-TIR

B2B

LaRD-1073 I2I

LaRD-1075 Rel. Geodetic

LaRD-1080 Absolute pointing 20 urad 13.4 meters 7.3 9.6 LNext SC Study SOW 22.6 18.7 Spacecraft IRD-326 SRD-425 Requirement Prediction Units Level 3 Units Requirement SRD-425 x x Pointing over 30 seconds (1 scene) 2 urad 1.3 meters 0.7 1.0 L9 S/C CDR 1.46 1.59 Spacecraft IRD-328 SRD-428 S/C ACS Performance Prediction Geodetic Accuracy - VSWIR 14.8 meters 30.0 meters CE90 LaRD-1078 CE90 SRD-428 x x x Pointing over 15 seconds (max band delay allowed) 1.5 urad 1.0 meters 0.6 0.7 L9 S/C CDR 0.343 0.343 Spacecraft IRD-329 SRD-429 S/C ACS Performance Prediction Geodetic Accuracy - TIR 17.7 meters 30.0 meters CE90 LaRD-1078 CE90 SRD-429 x x Ephemeris / Timing Geometric Accuracy (L1TP) 5.8 meters 8.0 meters CE90 LaRD-1082 CE90 SRD-422 x x Ephemeris knowledge 10 meters 9.0 meters 5.0 6.5 LNext SC Study SOW 2.5 2.5 Spacecraft IRD-320 SRD-422 Band Registration - VSWIR - 10m 2.0 meters 2.0 meters LE90 LaRD-1073 LE90 SRD-423 x x x Velocity knowledge 0.2 m/sec 0.18 m/sec 0.10 0.13 LNext SC Study SOW 0.0061 0.0061 Spacecraft IRD-321 SRD-423 Band Registration - VSWIR - 20m 2.4 meters 3.0 meters LE90 LaRD-1073 LE90 SRD-421 x x x Absolute timing knowledge 0.025 msec 0.17 meters 0.09 0.12 LNext SC Study SOW 0.01322 0.01322 Spacecraft IRD-319 SRD-421 Band Registration - VSWIR - 60m 5.0 meters 6.0 meters LE90 LaRD-1073 LE90 LIRD-299 x x x x Instrument clock uncertainty (VSWIR) 0.025 msec 0.17 meters 0.1 0.1 OLI-2 CDR 0.023 0.023 Instrument OLI-1214 LaRD-1216 Band Registration - TIR 5.6 meters 6.0 meters LE90 LaRD-1073 LE90 LIRD-301 x Instrument clock uncertainty (TIR) 0.025 msec 0.17 meters 0.1 0.1 TIRS-2 CDR 1.0 1.0 Instrument TIRS-563 LaRD-1216 Reflective to Thermal Band Registration 9.3 meters 15.0 meters LE90 LaRD-1073 LE90 SCIRD-271 x x x x x x Time tag uncertainty (VSWIR) 0.025 msec 0.17 meters 0.09 0.12 OLI-2 CDR 0.023 0.023 Instrument OLI-1214 LaRD-3423 Image Registration - VSWIR 3.1 meters 5.0 meters LE90 LaRD-1075 LE90 LaRD-2968 x x x x x x Time tag uncertainty (TIR) 0.025 msec 0.17 meters 0.09 0.12 OLI-2 CDR 0.023 0.023 Instrument OLI-1214 LaRD-3423 Relative Geodetic Accuracy - VSWIR 5.0 meters 9.0 meters CE90 LaRD-1080 CE90 LaRD-2970 x x On-orbit Stability / Knowledge LaRD-2971 x VSWIR Alignment stability (98 minutes) 12 urad 8.0 meters 4.4 5.7 L9 S/C CDR 14.84 12.4 Instrument IRD-454 LIRD-301 VSWIR mount to star tracker (ST on inst deck) Notes: LaRD-2975 x VSWIR Alignment stability (30 seconds) 1 urad 0.7 meters 0.4 0.5 L9 S/C CDR 1.02 1.06 Instrument IRD-453 LIRD-299 VSWIR mount to star tracker (ST on inst deck) 1. Started with the spacecraft knowledge and alignment specifications from the original LNext Spacecraft Study SOW. LaRD-1216 x x x x x x TIR to VSWIR alignment stability (98 minutes) 4 urad 2.7 meters 1.5 1.9 L9 S/C CDR 3.72 3.71 Instrument IRD-455 Allocation VSWIR mount to TIR mount - LandIS internal JItter and within-orbit LOS stability were tightened to meet the band-to-band requirement. LaRD-3423 x x x x x x VSWIR LOS relative knowledge (98 minutes) 2.4 urad 1.6 meters 0.9 1.1 LNext SC Study SOW 2.295 3.98 Instrument OLI-1113 LaRD-2968 Focal plane to Boresight (SOW was 5 urad) 2. Added knowledge, stability, and calibration requirements/allocations needed to build end-to-end performance budgets.

VSWIR boresight relative knowledge (98 minutes) 8 urad 5.4 meters 2.9 3.8 OLI-2 CDR 7.665 7.57 Instrument OLI-1115 LaRD-2970 Boresight to Mount Based upon L9 prelaunch best estimates from instrument and spacecraft vendors (L9 MCDR Estimate column), which VSWIR boresight relative knowledge (30 seconds) 1.5 urad 1.0 meters 0.6 0.7 OLI-2 CDR 1.848 2.78 Instrument Allocation Allocation Boresight to Mount were subsequently refined by comparison to observed on-orbit performance (L9 On-Orbit Estimate column).

VSWIR boresight rel. knowledge (max band delay) 1 urad 0.7 meters 0.4 0.5 OLI-2 CDR 0.333 0.332 Instrument Allocation Allocation Boresight to Mount 3. Band registration for the 10m bands is a driving requirement.

TIR LF LOS relative knowledge (98 minutes) 16 urad 10.7 meters 5.9 7.7 TIRS-2 CDR 21 20.8 Instrument TIRS-559 LaRD-2971 Low frequency (STOP) 4. Thermal band registration requirement is also tight.

TIR HF LOS relative knowledge (30 seconds) 8 urad 5.4 meters 2.9 3.8 L9 S/C CDR 5.804 5.93 Instrument TIRS-559 LaRD-2975 Spacecraft to TIRS-2 LOS jitter 5. Other end-to-end geometric requirements are not as stressing.

Spacecraft Jitter (to VSWIR LOS) 1.80 urad 1.2 meters 0.7 0.9 LNext SC Study SOW 0.518 0.515 Spacecraft IRD-3001 SCIRD-271 Spacecraft to OLI-2 LOS jitter (SOW was 2 urad) 6. No margin is included as this exercise is intended to demonstrate that the requirements are consistent, not to serve as Calibration a first draft design budget. Detailed vendor documentation will include design margin on the component requirements.

LOS knowledge focal plane-to-boresight (VSWIR) 3 urad 2.0 meters 1.1 1.4 L9 MCDR 3 2.87 Cal bration Allocation Allocation 7. (New) Changed 2.5 second pointing specification to 15 seconds based on expected maximum band-to-band delay.

LOS knowledge within focal plane (VSWIR) 1.5 urad 1.0 meters 0.6 0.7 L9 MCDR 1 1.15 Cal bration Allocation Allocation LOS knowledge (TIR to VSWIR) 10 urad 6.7 meters 3.7 4.8 LNext SC Study SOW 40 22.6 Cal bration Allocation Allocation LOS knowledge (TIR to TIR) 9 urad 6.0 meters 3.3 4.3 L9 MCDR 12 9.54 Cal bration Allocation Allocation Alignment knowledge (VSWIR to star tracker) 9 urad 6.0 meters 3.3 4.3 L9 MCDR 9 8.74 Cal bration Allocation Allocation

Methodology

5. Compare to the corresponding Level-2 and/or Level-3 requirement.

The end-to-end requirements come from the Level-2 (SMRD) and Level-3 (LandIS) requirements, and the spacecraft/instrument/ground system contributors were collected from the LNext SC Study SOW (shown in red text) and from L8/L9 estimates of actual performance. The method used was:

1. For each end-to-end performance characteristic, determine which spacecraft/instrument/ground system contributors apply and how (e.g., once, once per band, once per scene).

2. Rescale the 3-sigma contributors to 90% linear error (LE90) or 90% circular error (CE90), as appropriate for the end-to-end requirement, and scale to ground meters based upon the L10 orbital geometry.

3. Include additional (usually small) allocations for terrain knowledge effects, ground control/registration accuracy, and algorithm/modeling error, as appropriate to the individual end-to-end requirement.

4. Roll-up the rescaled contributors, usually by root-sum-square but in a few instances (e.g., alignment stability) by summing, to calculate predicted end-to-end performance.

Inputs and Summary

Geodetic Accuracy - VSWIR Allocation Spacecraft 3-sigma Units CE90 Units Notes Requirement Absolute pointing 20 urad 9.57 meters SRD-425 Ephemeris knowledge 10 meters 6.47 meters SRD-422 Absolute timing knowledge 0.025 msec 0.12 meters SRD-421 Spacecraft Jitter (to VSWIR LOS) 1.80 urad 0.86 meters SCIRD-271 Spacecraft Roll-Up 11.59 meters Instrument Instrument clock uncertainty (VSWIR) 0.025 msec 0.12 meters LaRD-1216 Time tag uncertainty (VSWIR) 0.025 msec 0.12 meters LaRD-3423 VSWIR Alignment stability (98 minutes) 12 urad 5.74 meters LIRD-301 VSWIR boresight relative knowledge (98 minutes) 8 urad 3.83 meters LaRD-2970 VSWIR LOS relative knowledge (98 minutes) 2.4 urad 1.15 meters LaRD-2968 Instrument Roll-Up 7.00 meters Ground Segment LOS knowledge focal plane-to-boresight (VSWIR) 3 urad 1.44 meters Calibration Allocation Alignment knowledge (VSWIR to star tracker) 9 urad 4.31 meters Calibration Allocation Band registration (20m VSWIR) 5.5 meters 3.91 meters LaRD-1073 Modeling budget 0.3 meters 0.21 meters Algorithms Allocation Ground Segment Roll-Up 6.00 meters Combined Roll-Up 14.8 meters Prediction L10 Level-3 Requirement 30.0 meters LaRD-1078

Geodetic Accuracy - TIR Allocation Spacecraft 3-sigma Units CE90 Units Notes Requirement Absolute pointing 20 urad 9.57 meters SRD-425 Absolute timing knowledge 0.025 msec 0.12 meters SRD-421 Ephemeris knowledge 10 meters 6.47 meters SRD-422 Spacecraft Roll-Up 11.56 meters Instrument Instrument clock uncertainty (TIR) 0.025 msec 0.12 meters LaRD-1216 Time tag uncertainty (TIR) 0.025 msec 0.12 meters LaRD-3423 TIR to VSWIR alignment stability (98 minutes) 4 urad 1.91 meters Allocation TIR LF LOS relative knowledge (98 minutes) 16 urad 7.66 meters LaRD-2971 TIR HF LOS relative knowledge (30 seconds) 8 urad 3.83 meters LaRD-2975 Instrument Roll-Up 8.78 meters Ground Segment LOS knowledge (TIR to VSWIR) 10 urad 4.79 meters Calibration Allocation Alignment knowledge (VSWIR to star tracker) 9 urad 4.31 meters Calibration Allocation Band registration (TIR) 10.9 meters 7.83 meters LaRD-1073 Modeling budget 0.3 meters 0.16 meters Algorithms Allocation Ground Segment Roll-Up 10.14 meters Combined Roll-Up 17.7 meters Prediction L10 Level-3 Requirement 30.0 meters LaRD-1078

Geometric Accuracy (L1TP) Allocation Spacecraft 3-sigma Units CE90 Units Notes Requirement Pointing over 30 seconds (1 scene) 2 urad 0.96 meters SRD-428 Spacecraft Jitter (to VSWIR LOS) 1.80 urad 0.86 meters SCIRD-271 Spacecraft Roll-Up 1.29 meters Instrument Instrument clock uncertainty (VSWIR) 0.025 msec 0.12 meters LaRD-1216 Time tag uncertainty (VSWIR) 0.025 msec 0.12 meters LaRD-3423 VSWIR Alignment stability (30 seconds) 1 urad 0.48 meters LIRD-299 VSWIR boresight relative knowledge (30 seconds) 1.5 urad 0.72 meters Allocation

Details

VSWIR LOS relative knowledge (98 minutes) 2.4 urad 1.15 meters LaRD-2968 Instrument Roll-Up 1.68 meters Ground LOS knowledge focal plane-to-boresight (VSWIR) 3 urad 1.44 meters Calibration Allocation Terrain error 11 meters 1.07 meters Edge of 14-deg FOV ESA DEM 6m LE90 Modeling budget 0.3 meters 0.21 meters Algorithms Allocation Band registration (20m VSWIR) 5.5 meters 3.91 meters LaRD-1073 Precision correction (GCP) budget 4.5 meters 3.22 meters Allocation Ground Roll-Up 5.38 meters Combined Roll-Up 5.8 meters Prediction L10 Level-3 Requirement 8.0 meters LaRD-1082

Band Registration - VSWIR - 10m Allocation Spacecraft 3-sigma Units LE90 Units Notes Requirement Pointing over 15 seconds (max band delay allowed) 1.50 urad 0.55 meters SRD-429 Velocity knowledge 0.2 m/sec 0.10 meters SRD-423 Absolute timing knowledge 0.025 msec 0.09 meters SRD-421 Jitter - Band 1 1.80 urad 0.66 meters SCIRD-271 Jitter - Band 2 1.80 urad 0.66 meters SCIRD-271 Spacecraft Roll-Up 1.09 meters Instrument Instrument clock uncertainty (VSWIR) - Band 1 0.025 msec 0.09 meters LaRD-1216 Time tag uncertainty (VSWIR) - Band 1 0.025 msec 0.09 meters LaRD-3423 Instrument clock uncertainty (VSWIR) - Band 2 0.025 msec 0.09 meters Error decorrelates over 15s LaRD-1216 Time tag uncertainty (VSWIR) - Band 2 0.025 msec 0.09 meters Error decorrelates over 15s LaRD-3423 VSWIR LOS relative knowledge (98 minutes) 2.4 urad 0.88 meters Count once LaRD-2968 Alignment stability (max band delay) 0.71 urad 0.26 meters Scaled from 30s LIRD-299 VSWIR boresight rel. knowledge (max band delay) 1.00 urad 0.37 meters Allocation Instrument Roll-Up 1.02 meters 6378137 Re Ground 7026320 Ro LOS knowledge within focal plane (VSWIR) 2.12 urad 0.78 meters Count twice Allocation 15 dT Terrain Induced Error 1.91 meters 1.05 meters 15 sec separation ESA DEM 6m LE90 5868.679 Tau Modeling budget - Band 1 0.3 meters 0.16 meters Algorithms Allocation 9.888 Angle Modeling budget - Band 2 0.3 meters 0.16 meters Algorithms Allocation 1.91 Parallax Ground Roll-Up 1.32 meters Combined Roll-Up 2.0 meters Prediction L10 Level-3 Requirement 2.0 meters 10m bands LaRD-1073

Band Registration - VSWIR - 20m Allocation Spacecraft 3-sigma Units LE90 Units Notes Requirement Pointing over 15 seconds (max band delay allowed) 1.50 urad 0.55 meters SRD-429 Velocity knowledge 0.2 m/sec 0.10 meters SRD-423 Absolute timing knowledge 0.025 msec 0.09 meters SRD-421 Jitter - Band 1 1.80 urad 0.66 meters SCIRD-271 Jitter - Band 2 1.80 urad 0.66 meters SCIRD-271 Spacecraft Roll-Up 1.09 meters Instrument Instrument clock uncertainty (VSWIR) - Band 1 0.025 msec 0.09 meters LaRD-1216 Time tag uncertainty (VSWIR) - Band 1 0.025 msec 0.09 meters LaRD-3423 Instrument clock uncertainty (VSWIR) - Band 2 0.025 msec 0.09 meters Error decorrelates over 15s LaRD-1216 Time tag uncertainty (VSWIR) - Band 2 0.025 msec 0.09 meters Error decorrelates over 15s LaRD-3423 VSWIR LOS relative knowledge (98 minutes) 2.4 urad 0.88 meters Count once LaRD-2968 Alignment stability (max band delay) 0.71 urad 0.26 meters Scaled from 30s LIRD-299 VSWIR boresight rel. knowledge (max band delay) 1.00 urad 0.37 meters Allocation Instrument Roll-Up 1.02 meters

Ground LOS knowledge within focal plane (VSWIR) 4.24 urad 1.56 meters Scaled to 20m Allocation Terrain Induced Error 1.91 meters 1.05 meters 15 sec separation ESA DEM 6m LE90 Modeling budget - Band 1 0.3 meters 0.16 meters Algorithms Allocation Modeling budget - Band 2 0.3 meters 0.16 meters Algorithms Allocation Ground Roll-Up 1.89 meters Combined Roll-Up 2.4 meters Prediction L10 Level-3 Requirement 3.0 meters 20m bands LaRD-1073

Band Registration - VSWIR - 60m Allocation Spacecraft 3-sigma Units LE90 Units Notes Requirement Pointing over 15 seconds (max band delay allowed) 1.50 urad 0.55 meters SRD-429 Velocity knowledge 0.2 m/sec 0.10 meters SRD-423 Absolute timing knowledge 0.025 msec 0.09 meters SRD-421 Jitter - Band 1 1.80 urad 0.66 meters SCIRD-271 Jitter - Band 2 1.80 urad 0.66 meters SCIRD-271 Spacecraft Roll-Up 1.09 meters Instrument Instrument clock uncertainty (VSWIR) - Band 1 0.025 msec 0.09 meters LaRD-1216 Time tag uncertainty (VSWIR) - Band 1 0.025 msec 0.09 meters LaRD-3423 Instrument clock uncertainty (VSWIR) - Band 2 0.025 msec 0.09 meters Error decorrelates over 15s LaRD-1216 Time tag uncertainty (VSWIR) - Band 2 0.025 msec 0.09 meters Error decorrelates over 15s LaRD-3423 VSWIR LOS relative knowledge (98 minutes) 2.4 urad 0.88 meters Count once LaRD-2968 Alignment stability (max band delay) 0.71 urad 0.26 meters Scaled from 30s LIRD-299 VSWIR boresight rel. knowledge (max band delay) 1.00 urad 0.37 meters Allocation Instrument Roll-Up 1.02 meters Ground LOS knowledge within focal plane (VSWIR) 12.73 urad 4.67 meters Scaled to 60m Allocation Terrain Induced Error 1.91 meters 1.05 meters 15 sec separation ESA DEM 6m LE90 Modeling budget - Band 1 0.3 meters 0.16 meters Algorithms Allocation Modeling budget - Band 2 0.3 meters 0.16 meters Algorithms Allocation Ground Roll-Up 4.79 meters Combined Roll-Up 5.0 meters Prediction L10 Level-3 Requirement 6.0 meters 60m bands LaRD-1073

Band Registration - TIR Allocation Spacecraft 3-sigma Units LE90 Units Notes Requirement Pointing over 15 seconds (max band delay allowed) 1.5 urad 0.55 meters SRD-429 Absolute timing knowledge 0.025 msec 0.09 meters SRD-421 Velocity knowledge 0.2 m/sec 0.10 meters SRD-423 Spacecraft Roll-Up 0.57 meters Instrument TIR alignment stability 4.00 urad 1.47 meters Allocation Instrument clock uncertainty (TIR) - Band 1 0.025 msec 0.09 meters LaRD-1216 Time tag uncertainty (TIR) - Band 1 0.025 msec 0.09 meters LaRD-3423 Instrument clock uncertainty (TIR) - Band 2 0.025 msec 0.09 meters Error decorrelates over 15s LaRD-1216 Time tag uncertainty (TIR) - Band 2 0.025 msec 0.09 meters Error decorrelates over 15s LaRD-3423 TIR HF LOS relative knowledge (30 seconds) 8 urad 2.94 meters LaRD-2975 TIR HF LOS relative knowledge (30 seconds) 8 urad 2.94 meters LaRD-2975 Instrument Roll-Up 4.41 meters Ground Terrain Induced Error 1.91 meters 1.05 meters 15 sec separation ESA DEM 6m LE90 LOS knowledge (TIR to TIR) 9.0 urad 3.30 meters Calibration Allocation Modeling budget - Band 1 0.3 meters 0.16 meters Algorithms Allocation Modeling budget - Band 2 0.3 meters 0.16 meters Algorithms Allocation

Ground Roll-Up 3.47 meters Combined Roll-Up 5.6 meters Prediction L10 Level-3 Requirement 6.0 meters 60m bands LaRD-1073

Reflective to Thermal Band Registration Allocation Spacecraft 3-sigma Units LE90 Units Notes Requirement Pointing over 15 seconds (max band delay allowed) 1.5 urad 0.55 meters SRD-429 Velocity knowledge 0.2 m/sec 0.10 meters SRD-423 Absolute timing knowledge 0.025 msec 0.09 meters SRD-421 Spacecraft Jitter (to VSWIR LOS) 1.80 urad 0.66 meters SCIRD-271 Spacecraft Roll-Up 0.87 meters Instrument Instrument clock uncertainty (VSWIR) 0.025 msec 0.09 meters LaRD-1216 Time tag uncertainty (VSWIR) 0.025 msec 0.09 meters LaRD-3423 Instrument clock uncertainty (TIR) 0.025 msec 0.09 meters LaRD-1216 Time tag uncertainty (TIR) 0.025 msec 0.09 meters LaRD-3423 TIR to VSWIR alignment stability (98 minutes) 4 urad 1.47 meters Allocation VSWIR LOS relative knowledge (98 minutes) 2.4 urad 0.88 meters LaRD-2968 VSWIR boresight relative knowledge (98 minutes) 8 urad 2.94 meters LaRD-2970 TIR LF LOS relative knowledge (98 minutes) 16 urad 5.87 meters LaRD-2971 TIR HF LOS relative knowledge (30 seconds) 8 urad 2.94 meters LaRD-2975 Instrument Roll-Up 7.74 meters Ground LOS knowledge focal plane-to-boresight (VSWIR) 3 urad 1.10 meters Calibration Allocation LOS knowledge within focal plane (VSWIR) 9 urad 3.30 meters Scaled to 60m Allocation LOS knowledge (TIR to VSWIR) 10 urad 3.67 meters Calibration Allocation Terrain Induced Error 1.91 meters 1.05 meters 20 sec separation ESA DEM 6m LE90 Modeling budget - VSWIR 0.3 meters 0.16 meters Algorithms Allocation Modeling budget - TIR 0.3 meters 0.16 meters Algorithms Allocation Ground Roll-Up 5.17 meters Combined Roll-Up 9.3 meters RSS Prediction L10 Level-3 Requirement 15.0 meters LaRD-1073

Image Registration - VSWIR Allocation Spacecraft 3-sigma Units LE90 Units Notes Requirement Pointing over 30 seconds (1 scene) - Scene 1 2 urad 0.73 meters SRD-428 Spacecraft Jitter (to VSWIR LOS) - Scene 1 1.80 urad 0.66 meters SCIRD-271 Pointing over 30 seconds (1 scene) - Scene 2 2 urad 0.73 meters SRD-428 Spacecraft Jitter (to VSWIR LOS) - Scene 2 1.80 urad 0.66 meters SCIRD-271 Spacecraft Roll-Up 1.40 meters Instrument Instrument clock uncertainty (VSWIR) - Scene 1 0.025 msec 0.09 meters LaRD-1216 Time tag uncertainty (VSWIR) - Scene 1 0.025 msec 0.09 meters LaRD-3423 Alignment stability (30 sec) - Scene 1 1 urad 0.37 meters LIRD-299 VSWIR internal stability (30 seconds) - Scene 1 1.5 urad 0.55 meters Allocation VSWIR LOS relative knowledge (98 minutes) - Scene 1 2.4 urad 0.88 meters LaRD-2968 Instrument clock uncertainty (VSWIR) - Scene 2 0.025 msec 0.09 meters LaRD-1216 Time tag uncertainty (VSWIR) - Scene 2 0.025 msec 0.09 meters LaRD-3423 Alignment stability (30 sec) - Scene 2 1 urad 0.37 meters LIRD-299 VSWIR internal stability (30 seconds) - Scene 2 1.5 urad 0.55 meters Allocation VSWIR LOS relative knowledge (98 minutes) - Scene 2 2.4 urad 0.88 meters LaRD-2968 Instrument Roll-Up 1.82 meters Ground LOS knowledge focal plane-to-boresight (VSWIR) - Scene 1 3 urad 1.10 meters Allocation LOS knowledge focal plane-to-boresight (VSWIR) - Scene 2 3 urad 1.10 meters Allocation Modeling budget - Scene 1 0.3 meters 0.16 meters Algorithms Allocation

Modeling budget - Scene 2 0.3 meters 0.16 meters Algorithms Allocation Registration processing budget 2.5 meters 1.37 meters 0.25 pixel Allocation Ground Roll-Up 2.09 meters Combined Roll-Up 3.1 meters Prediction L10 Level-3 Requirement 5.0 meters LaRD-1075

Relative Geodetic Accuracy - VSWIR Allocation Spacecraft 3-sigma Units CE90 Units Notes Requirement Absolute pointing 20 urad 1.36 meters Yaw only SRD-425 Pointing over 30 seconds (1 scene) 2 urad 0.96 meters SRD-428 Ephemeris knowledge 10 meters 0.92 meters Z only SRD-422 Velocity knowledge 0.2 m/sec 0.13 meters SRD-423 Spacecraft Jitter (to VSWIR LOS) 1.8 urad 0.86 meters SCIRD-271 Spacecraft Roll-Up 2.09 meters Instrument Instrument clock uncertainty (VSWIR) 0.025 msec 0.12 meters LaRD-1216 Time tag uncertainty (VSWIR) 0.025 msec 0.12 meters LaRD-3423 VSWIR Alignment stability (30 seconds) 1 urad 0.48 meters LIRD-299 VSWIR boresight relative knowledge (30 seconds) 1.5 urad 0.72 meters Allocation VSWIR LOS relative knowledge (98 minutes) 2.4 urad 1.15 meters LaRD-2968 Instrument Roll-Up 1.68 meters Ground LOS knowledge focal plane-to-boresight (VSWIR) 3 urad 1.44 meters Calibration Allocation Alignment knowledge (VSWIR to star tracker) 9 urad 0.61 meters Yaw only Allocation Band registration (VSWIR) 5.5 meters 3.91 meters LaRD-1073 Modeling budget 0.3 meters 0.21 meters Algorithms Allocation Ground Segment Roll-Up 4.22 meters Combined Roll-Up 5.0 meters Prediction L10 Level-3 Requirement 9.0 meters LaRD-1080

Image Registration - TIR Allocation Spacecraft 3-sigma Units LE90 Units Requirement Pointing over 30 seconds (1 scene) - Scene 1 2 urad 0.73 meters SRD-428 Pointing over 30 seconds (1 scene) - Scene 2 2 urad 0.73 meters SRD-428 Spacecraft Roll-Up 1.04 meters Instrument Instrument clock uncertainty (TIR) - Scene 1 0.025 msec 0.09 meters LaRD-1216 Time tag uncertainty (TIR) - Scene 1 0.025 msec 0.09 meters LaRD-3423 TIR to VSWIR alignment stability (98 minutes) - Scene 1 4 urad 1.47 meters Allocation TIR LF LOS relative knowledge (98 minutes) - Scene 1 16 urad 5.87 meters LaRD-2971 Instrument clock uncertainty (TIR) - Scene 2 0.025 msec 0.09 meters LaRD-1216 Time tag uncertainty (TIR) - Scene 2 0.025 msec 0.09 meters LaRD-3423 TIR to VSWIR alignment stability (98 minutes) - Scene 2 4 urad 1.47 meters Allocation TIR LF LOS relative knowledge (98 minutes) - Scene 2 16 urad 5.87 meters LaRD-2971 Instrument Roll-Up 8.56 meters Ground LOS knowledge (TIR to TIR) - Scene 1 9 urad 3.3 meters Allocation LOS knowledge (TIR to TIR) - Scene 2 9 urad 3.3 meters Allocation Modeling budget - Scene 1 0.3 meters 0.2 meters Algorithms Allocation Modeling budget - Scene 2 0.3 meters 0.2 meters Algorithms Allocation Registration processing budget 15 meters 8.2 meters 0.25 pixel Allocation Ground Roll-Up 9.46 meters Combined Roll-Up 12.8 meters Prediction