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  • 1
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    The GOES-16 Spacecraft Science Magnetometer (2019)
    Springer
    Details
    Publication Date: 2019-05-16
    Print ISSN: 0038-6308
    Electronic ISSN: 1572-9672
    Topics: Physics
    Published by Springer
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    PAPER CURRENT
  • 2
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    Correcting the Arcjet Thruster Disturbance in GOES‐16 Magnetometer Data (2020)
    American Geophysical Union
    Details
    Publication Date: 2020-01-01
    Print ISSN: 1542-7390
    Electronic ISSN: 1542-7390
    Topics: Geosciences , Physics
    Published by American Geophysical Union
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    PAPER CURRENT
  • 3
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    Attitude analysis of the Earth Radiation Budget Satellite (ERBS) yaw turn anomaly (1988)
    In:  CASI
    Details
    Publication Date: 2013-08-31
    Description: The July 2 Earth Radiation Budget Satellite (ERBS) hydrazine thruster-controlled yaw inversion maneuver resulted in a 2.1 deg/sec attitude spin. This mode continued for 150 minutes until the spacecraft was inertially despun using the hydrazine thrusters. The spacecraft remained in a low-rate Y-axis spin of .06 deg/sec for 3 hours until the B-DOT control mode was activated. After 5 hours in this mode, the spacecraft Y-axis was aligned to the orbit normal, and the spacecraft was commanded to the mission mode of attitude control. This work presents the experience of real-time attitude determination support following analysis using the playback telemetry tape recorded for 7 hours from the start of the attitude control anomaly.
    Keywords: ASTRODYNAMICS
    Type: NASA, Goddard Space Flight Center, Flight Mechanics(Estimation Theory Symposium 1988; p 368-390
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 4
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    Post Launch Calibration and Testing of the Advanced Baseline Imager on the GOES-R Satellite (2016)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: The Geostationary Operational Environmental Satellite R (GOES-R) series is the planned next generation of operational weather satellites for the United States National Oceanic and Atmospheric Administration. The first launch of the GOES-R series is planned for October 2016. The GOES-R series satellites and instruments are being developed by the National Aeronautics and Space Administration (NASA). One of the key instruments on the GOES-R series is the Advance Baseline Imager (ABI). The ABI is a multi-channel, visible through infrared, passive imaging radiometer. The ABI will provide moderate spatial and spectral resolution at high temporal and radiometric resolution to accurately monitor rapidly changing weather. Initial on-orbit calibration and performance characterization is crucial to establishing baseline used to maintain performance throughout mission life. A series of tests has been planned to establish the post launch performance and establish the parameters needed to process the data in the Ground Processing Algorithm. The large number of detectors for each channel required to provide the needed temporal coverage presents unique challenges for accurately calibrating ABI and minimizing striping. This paper discusses the planned tests to be performed on ABI over the six-month Post Launch Test period and the expected performance as it relates to ground tests.
    Keywords: Earth Resources and Remote Sensing; Meteorology and Climatology; Instrumentation and Photography
    Type: GSFC-E-DAA-TN30958 , SPIE Asia-Pacific Remote Sensing; Apr 04, 2016 - Apr 07, 2016; New Dehli; India
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 5
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    Lessons Learned from Flight Observations of the GOES-R Magnetometer (2019)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: The Geostationary Operational Environmental Satellite (GOES)-16 observatory was launched on 19 November 2016. During daily on-orbit operations, shadowing of the inboard magnetometer sensor unit occurs due to spacecraft geometry and solar angle. Throughout the shadowing periods of the inboard magnetometer, anomalous excursions of 20 nanotesla (nT) are observed. In addition to the excursions during shadow events, the measurement difference between the inboard and outboard magnetometer varies over the day, indicating erroneous measurements by one or both magnetometers. In addition, based on the deployment rotations, the zero offsets of the X and Y axes were found to be significantly different, ~30nT, from ground calibration data. Because of these observations, an extensive root cause investigation was undertaken to correct the magnetometer system for the next spacecraft in the GOES-R series. This paper documents the efforts of that activity and the lessons learned as a result of the investigation.
    Keywords: Earth Resources and Remote Sensing
    Type: GSFC-E-DAA-TN68765 , 2019 ESA Workshop on Aerospace EMC; May 20, 2019 - May 22, 2019; Budapest; Hungary
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 6
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    Post Launch Calibration and Testing of the Advanced Baseline Imager on the GOES-R Satellite (2016)
    In:  CASI
    Details
    Publication Date: 2019-08-13
    Description: The Geostationary Operational Environmental Satellite R (GOES-R) series is the planned next generation of operational weather satellites for the United State's National Oceanic and Atmospheric Administration. The first launch of the GOES-R series is planned for October 2016. The GOES-R series satellites and instruments are being developed by the National Aeronautics and Space Administration (NASA). One of the key instruments on the GOES-R series is the Advance Baseline Imager (ABI). The ABI is a multi-channel, visible through infrared, passive imaging radiometer. The ABI will provide moderate spatial and spectral resolution at high temporal and radiometric resolution to accurately monitor rapidly changing weather. Initial on-orbit calibration and performance characterization is crucial to establishing baseline used to maintain performance throughout mission life. A series of tests has been planned to establish the post launch performance and establish the parameters needed to process the data in the Ground Processing Algorithm. The large number of detectors for each channel required to provide the needed temporal coverage presents unique challenges for accurately calibrating ABI and minimizing striping. This paper discusses the planned tests to be performed on ABI over the six-month Post Launch Test period and the expected performance as it relates to ground tests.
    Keywords: Earth Resources and Remote Sensing; Instrumentation and Photography; Meteorology and Climatology
    Type: GSFC-E-DAA-TN30825 , SPIE Asia-Pacific Remote Sensing; Apr 03, 2016 - Apr 07, 2016; New Delhi; India
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 7
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    Lessons Learned from Flight Observations of the GOES-R Magnetometer (2019)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: The Geostationary Operational Environmental Satellite (GOES)-16 observatory was launched on 19 November 2016. During daily on-orbit operations, shadowing of the inboard magnetometer sensor unit occurs due to spacecraft geometry and solar angle. Throughout the shadowing periods of the inboard magnetometer, anomalous excursions of 20 nanotesla (nT) are observed. In addition to the excursions during shadow events, the measurement difference between the inboard and outboard magnetometer varies over the day, indicating erroneous measurements by one or both magnetometers. In addition, based on the deployment rotations, the zero offsets of the X and Y axes were found to be significantly different, ~30nT, from ground calibration data. Because of these observations, an extensive root cause investigation was undertaken to correct the magnetometer system for the next spacecraft in the GOES-R series. This paper documents the efforts of that activity and the lessons learned as a result of the investigation.
    Keywords: Earth Resources and Remote Sensing
    Type: GSFC-E-DAA-TN64892 , 2019 ESA Workshop on Aerospace EMC; May 20, 2019 - May 22, 2019; Budapest; Hungary
    Format: application/pdf
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    NASA TECHNICAL REPORTS
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