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Design and Execution of Dawn HAMO to LAMO Transfer at CeresOn October 23, 2015, the Dawn spacecraft left the High Altitude Mapping Orbit (HAMO) around Ceres and began its final decent to the Low Altitude Mapping Orbit (LAMO), arriving on December 15. The transfer between the two science orbits, a tight spiraling trajectory with over 100 revolutions, required the operations team to perform weekly maneuver designs for a period of 50 days. While the first six weeks of the transfer executed as planned, unexpectedly the spacecraft incurred a multi-sigma delivery error to the final science orbit that was subsequently clean-up at the first orbit maintenance maneuver. In this paper we discuss the design architecture for the transfer in detail, including challenges the team faced in flying the transfer and lessons learned.
Document ID
20200000153
Acquisition Source
Jet Propulsion Laboratory
Document Type
Presentation
External Source(s)
Authors
Grebow, Dan
(Jet Propulsion Laboratory (JPL), California Institute of Technology (CalTech) Pasadena, CA, United States)
Date Acquired
January 7, 2020
Publication Date
September 13, 2016
Subject Category
Astrodynamics
Report/Patent Number
JPL-CL-16-4171
Report Number: JPL-CL-16-4171
Meeting Information
Meeting: AIAA/AAS Astrodynamics Specialist Conference
Location: Long Beach, CA
Country: United States
Start Date: September 13, 2016
End Date: September 16, 2016
Sponsors: American Institute of Aeronautics and Astronautics (AIAA), American Astronomical Society
Distribution Limits
Public
Copyright
Other

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