Multi-arc filtering during the navigation campaign of the osiris-rex mission

Andrew S. French, Jason M. Leonard, Jeroen L. Geeraert, Brian R. Page, Peter G. Antreasian, Michael C. Moreau, Jay W. McMahon, Daniel J. Scheeres, Dante S. Lauretta

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

The Navigation Campaign of the OSIRIS-REx mission consisted of three phases: Approach, Preliminary Survey and Orbital A. These phases were designed to optimize the initial characterization of Bennu’s mass, shape and spin state to support a safe orbit insertion and a quick transition to landmark-based optical navigation tracking. The standard orbit determination filtering techniques used to navigate the spacecraft were unable to fit data from these three phases simultaneously due to numerical issues associated with the nonlinear dynamics and the long arc length. Consequently, a multi-arc filtering algorithm was implemented in order to combine the information from each of these arcs. Multi-arc solutions for Bennu’s spin state and gravity field are presented here.

Original languageEnglish (US)
Title of host publicationAAS/AIAA Astrodynamics Specialist Conference, 2019
EditorsKenneth R. Horneman, Christopher Scott, Brian W. Hansen, Islam I. Hussein
PublisherUnivelt Inc.
Pages3051-3068
Number of pages18
ISBN (Print)9780877036654
StatePublished - 2020
EventAAS/AIAA Astrodynamics Specialist Conference, 2019 - Portland, United States
Duration: Aug 11 2019Aug 15 2019

Publication series

NameAdvances in the Astronautical Sciences
Volume171
ISSN (Print)0065-3438

Conference

ConferenceAAS/AIAA Astrodynamics Specialist Conference, 2019
CountryUnited States
CityPortland
Period8/11/198/15/19

ASJC Scopus subject areas

  • Aerospace Engineering
  • Space and Planetary Science

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