Osiris-rex orbit determination performance during the navigation campaign

Jason M. Leonard; Jeroen L. Geeraert; Brian R. Page; Andrew S. French; Peter G. Antreasian; Coralie D. Adam; Daniel R. Wibben; Michael C. Moreau; Dante S. Lauretta

Osiris-rex orbit determination performance during the navigation campaign

Jason M. Leonard, Jeroen L. Geeraert, Brian R. Page, Andrew S. French, Peter G. Antreasian, Coralie D. Adam, Daniel R. Wibben, Michael C. Moreau, Dante S. Lauretta

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

2 Scopus citations

Abstract

The OSIRIS-REx mission Navigation Campaign consists of three sub-phases: Approach, Preliminary Survey, and Orbital A. Approach was designed for initial characterization of Bennu while matching Bennu’s heliocentric velocity. Preliminary Survey provided the first spacecraft-based estimate of Bennu’s mass. This phase consisted of five target flybys with a close approach distance of about 7 km. Orbital A was a two-month phase devoted to the Navigation Team learning the close proximity operations dynamics and environment around Bennu and transitioning from center-finding optical navigation to landmark feature-based navigation. This paper provides a detailed summary of the orbit determination performance throughout the Navigation Campaign.

Original language	English (US)
Title of host publication	AAS/AIAA Astrodynamics Specialist Conference, 2019
Editors	Kenneth R. Horneman, Christopher Scott, Brian W. Hansen, Islam I. Hussein
Publisher	Univelt Inc.
Pages	3031-3050
Number of pages	20
ISBN (Print)	9780877036654
State	Published - 2020
Event	AAS/AIAA Astrodynamics Specialist Conference, 2019 - Portland, United States Duration: Aug 11 2019 → Aug 15 2019

Publication series

Name	Advances in the Astronautical Sciences
Volume	171
ISSN (Print)	0065-3438

Conference

Conference	AAS/AIAA Astrodynamics Specialist Conference, 2019
Country/Territory	United States
City	Portland
Period	8/11/19 → 8/15/19

ASJC Scopus subject areas

Aerospace Engineering
Space and Planetary Science

Cite this

Leonard, J. M., Geeraert, J. L., Page, B. R., French, A. S., Antreasian, P. G., Adam, C. D., Wibben, D. R., Moreau, M. C., & Lauretta, D. S. (2020). Osiris-rex orbit determination performance during the navigation campaign. In K. R. Horneman, C. Scott, B. W. Hansen, & I. I. Hussein (Eds.), AAS/AIAA Astrodynamics Specialist Conference, 2019 (pp. 3031-3050). (Advances in the Astronautical Sciences; Vol. 171). Univelt Inc..

Osiris-rex orbit determination performance during the navigation campaign. / Leonard, Jason M.; Geeraert, Jeroen L.; Page, Brian R. et al.
AAS/AIAA Astrodynamics Specialist Conference, 2019. ed. / Kenneth R. Horneman; Christopher Scott; Brian W. Hansen; Islam I. Hussein. Univelt Inc., 2020. p. 3031-3050 (Advances in the Astronautical Sciences; Vol. 171).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Leonard, JM, Geeraert, JL, Page, BR, French, AS, Antreasian, PG, Adam, CD, Wibben, DR, Moreau, MC & Lauretta, DS 2020, Osiris-rex orbit determination performance during the navigation campaign. in KR Horneman, C Scott, BW Hansen & II Hussein (eds), AAS/AIAA Astrodynamics Specialist Conference, 2019. Advances in the Astronautical Sciences, vol. 171, Univelt Inc., pp. 3031-3050, AAS/AIAA Astrodynamics Specialist Conference, 2019, Portland, United States, 8/11/19.

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abstract = "The OSIRIS-REx mission Navigation Campaign consists of three sub-phases: Approach, Preliminary Survey, and Orbital A. Approach was designed for initial characterization of Bennu while matching Bennu{\textquoteright}s heliocentric velocity. Preliminary Survey provided the first spacecraft-based estimate of Bennu{\textquoteright}s mass. This phase consisted of five target flybys with a close approach distance of about 7 km. Orbital A was a two-month phase devoted to the Navigation Team learning the close proximity operations dynamics and environment around Bennu and transitioning from center-finding optical navigation to landmark feature-based navigation. This paper provides a detailed summary of the orbit determination performance throughout the Navigation Campaign.",

author = "Leonard, {Jason M.} and Geeraert, {Jeroen L.} and Page, {Brian R.} and French, {Andrew S.} and Antreasian, {Peter G.} and Adam, {Coralie D.} and Wibben, {Daniel R.} and Moreau, {Michael C.} and Lauretta, {Dante S.}",

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AU - Page, Brian R.

AU - French, Andrew S.

AU - Antreasian, Peter G.

AU - Adam, Coralie D.

AU - Wibben, Daniel R.

AU - Moreau, Michael C.

AU - Lauretta, Dante S.

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AB - The OSIRIS-REx mission Navigation Campaign consists of three sub-phases: Approach, Preliminary Survey, and Orbital A. Approach was designed for initial characterization of Bennu while matching Bennu’s heliocentric velocity. Preliminary Survey provided the first spacecraft-based estimate of Bennu’s mass. This phase consisted of five target flybys with a close approach distance of about 7 km. Orbital A was a two-month phase devoted to the Navigation Team learning the close proximity operations dynamics and environment around Bennu and transitioning from center-finding optical navigation to landmark feature-based navigation. This paper provides a detailed summary of the orbit determination performance throughout the Navigation Campaign.

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Osiris-rex orbit determination performance during the navigation campaign

Abstract

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ASJC Scopus subject areas

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