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The use of laser altimetry in the orbit and attitude determination of Mars Global Surveyor
Author(s) -
Rowlands D. D.,
Pavlis D. E.,
Lemoine F. G.,
Neumann G. A.,
Luthcke S. B.
Publication year - 1999
Publication title -
geophysical research letters
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 2.007
H-Index - 273
eISSN - 1944-8007
pISSN - 0094-8276
DOI - 10.1029/1999gl900223
Subject(s) - altimeter , mars exploration program , geodesy , orbit determination , orbit (dynamics) , remote sensing , geology , spacecraft , crossover , terrain , mars landing , exploration of mars , aerospace engineering , satellite , computer science , physics , geography , astrobiology , engineering , cartography , artificial intelligence
Altimetry from the Mars Observer Laser Altimeter (MOLA), an instrument on board the Mars Global Surveyor (MGS) spacecraft, has been analyzed for the period of the MGS Science Phasing Orbit‐1 (SPO‐1) mission phase. Altimeter ranges have been used to improve significantly the orbit and attitude knowledge of the spacecraft by the use of crossover constraint equations derived from short passes of the MOLA data. These constraint equations differ from traditional crossover constraints and exploit the small footprint associated with laser altimetry. The rationale for using this technique with laser altimetry over sloping terrain is laid out and evidence of the resulting benefit is presented.