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Attitude Ground System: Recent Experiences in Attitude Sensor Calibration and Upcoming Mission Support for Momentum UnloadingA key component of the mission ground system used for supporting NASA Goddard Space Flight Center space missions, known as the Attitude Ground System (AGS), is used to perform operational and analytical support for the spacecraft attitude con-trol system (ACS). The AGS is comprised of a real-time attitude analysis and moni-toring system, and a tool for performing offline analysis of the ACS system using key sensor telemetry collected and stored onboard and transmitted to the mission operations center. The AGS performs numerous functions, including independent ground attitude determination, attitude slew planning and commanding, attitude sensor calibration, and real-time monitoring of the health and safety of the ACS. The AGS is developed in MATLAB using a core library of utility functions called the Multi-Mission Three-Axis Satellite System (MTASS). The MTASS library has been used to support mission operations for over thirty NASA missions starting in the late 1990s. It is customized for each mission to meet specific mission requirements. In this paper we describe recent operational experience using the AGS to support the launch and early orbit (L&EO) phase of the Plankton, Aerosol, Cloud Ocean Ecosys-tem (PACE) and Joint Polar Satellite System (JPSS) missions. Our summary of L&EO support for PACE and JPSS includes ACS sensor calibration of the alignment and scale factors for the Star Trackers, Inertial Reference Unit, and Three-Axis Magnetometers. We will also describe new capabilities for planning and executing reaction wheel momentum unloading for the Roman Space Telescope (RST) During the spacecraft early orbit phase, the AGS is operated in the mission operations center by a team of subject matter experts that also develop and configure the AGS soft-ware. This unique approach, integrating system development and operation in a sin-gle engineering team, provides valuable expertise for quick assessment of ACS per-formance and safety; critical to anomaly resolution and mission success.
Document ID
20250000951
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Philip C Calhoun
(Goddard Space Flight Center Greenbelt, United States)
Jonathan Glickman
(AI Solutions Lanham, Maryland, United States)
Richard Harman
(AI Solutions Lanham, Maryland, United States)
Joseph Sedlak
(AI Solutions Lanham, Maryland, United States)
Date Acquired
January 24, 2025
Subject Category
Spacecraft Design, Testing and Performance
Meeting Information
Meeting: 47th American Astronautical Society (AAS) Guidance, Navigation and Control GN&C Conference
Location: Breckenridge, CO
Country: US
Start Date: January 31, 2025
End Date: February 5, 2025
Sponsors: American Astronautical Society
Funding Number(s)
WBS: 134180.06.06.07.01
CONTRACT_GRANT: 80GSFC19C0072
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
Guidance, Navigation, and Control
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