Osiris-rex navigation campaign trajectory design and maneuver performance

Daniel R. Wibben, Andrew Levine, Samantha Rieger, James V. McAdams, Peter Antreasian, Jason M. Leonard, Michael C. Moreau, Dante S. Lauretta

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

Abstract

The first six months of asteroid proximity operations for the OSIRIS-REx mission is known as the Navigation Campaign – a portion of the mission designed to optimize initial characterization of asteroid Bennu and its dynamical environment in support of initial orbit insertion and transition from star-based to landmark-based optical navigation. During this time, the spacecraft executed 16 maneuvers across a large range of AV magnitudes. This work discusses the spacecraft trajectory design of the Navigation Campaign, which enabled the collection of critical information that led to the achievement of these milestones, A and a summary of the performance of executed maneuvers.

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.
Pages2945-2958
Number of pages14
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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