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Dawn Orbit Determination Team: Modeling and Fitting of Optical Data at VestaThe Dawn spacecraft was launched on September 27th, 2007. Its mission is to consecutively rendezvous with and observe the two largest bodies in the main asteroid belt, Vesta and Ceres. It has already completed over a year's worth of direct observations of Vesta (spanning from early 2011 through late 2012) and is currently on a cruise trajectory to Ceres, where it will begin scientific observations in mid-2015. Achieving this data collection required careful planning and execution from all Dawn operations teams. Dawn's Orbit Determination (OD) team was tasked with reconstruction of the as-flown trajectory as well as determination of the Vesta rotational rate, pole orientation and ephemeris, among other Vesta parameters. Improved knowledge of the Vesta pole orientation, specifically, was needed to target the final maneuvers that inserted Dawn into the first science orbit at Vesta. To solve for these parameters, the OD team used radiometric data from the Deep Space Network (DSN) along with optical data reduced from Dawn's Framing Camera (FC) images. This paper will de-scribe the initial determination of the Vesta ephemeris and pole using a combination of radiometric and optical data, and also the progress the OD team has made since then to further refine the knowledge of Vesta's body frame orientation and rate with these data.
Document ID
20150007247
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Kennedy, Brian
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Abrahamson, Matt
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Ardito, Alessandro
(ARPSOFT S.r.l. Rome, Italy)
Haw, Robert
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Mastrodemos, Nicholas
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Nandi, Sumita
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Park, Ryan
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Rush, Brian
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Vaughan, Andrew
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
May 4, 2015
Publication Date
February 10, 2013
Subject Category
Astrodynamics
Report/Patent Number
AAS 13-347
Meeting Information
Meeting: AAS/AIAA Spaceflight Mechanics Meeting
Location: Kauai, HI
Country: United States
Start Date: February 10, 2013
End Date: February 14, 2013
Sponsors: American Astronautical Society, American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Other
Keywords
imagery
low thrust
optical navigation
asteroid encounter

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