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Orbit Determination Strategy and Simulation Performance for OSIRIS-REx Proximity OperationsThe Origins Spectral Interpretation Resource Identification Security Regolith Explorer (OSIRISREx)is a NASA New Frontiers mission to the near-earth asteroid Bennu that will rendez vousin 2018, create a comprehensive and detailed set of observations over several years, collect a regolith sample, and return the sample to Earth in 2023. The Orbit Determination (OD) team isa sub-section of the Flight Dynamics System responsible for generating precise reconstructions and predictions of the spacecraft trajectory. The OD team processes radiometric data, LIDAR, as well as center-finding and landmark-based Optical Navigation images throughout the proximity operations phase to estimate and predict the spacecraft location within several meters. Stringent knowledge requirements stress the OD teams concept of operations and procedures to produce verified and consistent high quality solutions for observation planning, maneuver planning, and onboard sequencing. This paper will provide insight into the OD concept of operations and summarize the OD performance expected during the approach and early proximity operation phases,based on our pre-encounter knowledge of Bennu. Strategies and methods used to compare and evaluate predicted and reconstructed solutions are detailed. The use of high fidelity operational tests during early 2017 will stress the teams concept of operations and ability to produce precise OD solutions with minimal turn-around delay.
Document ID
20170011463
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Leonard, Jason M.
(KinetX Aerospace, Inc Simi Valley, CA, United States)
Antreasian, Peter G.
(KinetX Aerospace, Inc Simi Valley, CA, United States)
Jackman, Coralie D.
(KinetX Aerospace, Inc Simi Valley, CA, United States)
Page, Brian
(KinetX Aerospace, Inc Simi Valley, CA, United States)
Wibben, Daniel R.
(KinetX Aerospace, Inc Simi Valley, CA, United States)
Moreau, Michael C.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
December 1, 2017
Publication Date
May 29, 2017
Subject Category
Astrodynamics
Report/Patent Number
GSFC-E-DAA-TN42967
GSFC-E-DAA-TN43068
Meeting Information
Meeting: International ESA Conference on Guidance, Navigation and Control Systems
Location: Salzburg
Country: Austria
Start Date: May 29, 2017
End Date: June 2, 2017
Sponsors: European Space Agency
Funding Number(s)
CONTRACT_GRANT: NNG13FC02C
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Technical Management
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