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Ulysses orbit determinationThe Ulysses mission ESA spacecraft with ESA and NASA experiments explores the polar regions of the sun by sending a spacecraft on a trajectory out of the ecliptic after a Jupiter flyby. After correcting for launch errors and refining the aimpoint, orbit determination results show the change and general improvement in the Jupiter arrival point. Orbit determination results are further discussed, and future plans are mentioned.
Document ID
19920060687
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gordon, H. J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Luthey, J. L.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Mcelrath, T. P.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Menon, P. R.
(JPL Pasadena, CA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Subject Category
Astrodynamics
Report/Patent Number
AAS PAPER 91-472
Report Number: AAS PAPER 91-472
Meeting Information
Meeting: AAS/AIAA Astrodynamics Conference
Location: Durango, CO
Country: United States
Start Date: August 19, 1991
End Date: August 22, 1991
Accession Number
92A43311
Distribution Limits
Public
Copyright
Other

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