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High Fidelity Reconstructed Attitude Estimation Using Cassini Flight TelemetryThe Cassini Grand Finale capped the 20 year Cassini mission with 22 one-week-long orbits each with periapsis inside the ring plane just above Saturn’s cloud tops. One aspect of these remarkable orbits was unprecedented measurements of Saturn’s magnetic field very close to the planet. Processing this data required precise estimates of Cassini’s orientation during these ring plane crossings. These periods coincided with planned gyro-only attitude propagation due to the enormous bright bodies in the star tracker field-of-view. This paper describes how attitude reacquisition information, when the star tracker reacquires an absolute inertial reference, can be used to correct errors introduced during gyro-only propagation. The resulting high fidelity reconstruction significantly improves the extraction of Saturn’s magnetic field from the raw data obtained during gyro-only periods when Cassini’s changing orientation makes precise attitude estimation a challenge.



Document ID
20190028439
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Burk, Thomas A.
(Jet Propulsion Laboratory, California Institute of Technology (JPL/CalTech) Pasadena, CA, United States)
Date Acquired
August 1, 2019
Publication Date
January 1, 2018
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Report/Patent Number
JPL-CL-CL#17-6210
Report Number: JPL-CL-CL#17-6210
Meeting Information
Meeting: AIAA Science and Technology Forum and Exposition (AIAA SciTech 2018)
Location: Kissimmee, FL
Country: United States
Start Date: January 8, 2018
End Date: January 12, 2018
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Distribution Limits
Public
Copyright
Other

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