Optimal Control of Spacecraft Motion in the Newtonian Gravitational Field: Application of Quaternions to Describe Orbit Orientation

Details Optimal Control of Spacecraft Motion in the Newtonian Gravitational Field: Application of Quaternions to Describe Orbit Orientation Optimal Control of Spacecraft Motion in the Newtonian Gravitational Field: Application of Quaternions to Describe Orbit Orientation

Jul 1999

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1999cosre..37..409c&link_type=openurl

Cosmic Research, Vol. 37, No. 4, p.409

Physics

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