AGI Technology Beyond Earth Orbit

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HPOP in STK vs.ODTK• ODTK’s Earth.cb settings– Nutation Method, Nutation Update Interval• Gauss-Markov processes– STK/HPOP supports propagation• Hidden: No GUI or report– STK/ASTG doesn’t support this• Multiple eclipse bodies– Can’t configure yet in STK/HPOP• Hidden: No Gui (STK 8.2!)– Can configure in STK/ASTG• 3 rd Body mu values– ODTK uses CB file value only (not configurable)• Astro Consistency doc in ODTK Help (HPOP/ASTG)AGIPg 38 of 40www.agi.com
Future direction (Woodburn)• HPOP – ASTG merge• Additional DSN measurement models• Mars GRAM• Additional SPICE integration• What else should we be doing?AGIPg 39 of 40www.agi.com
Page 1 and 2: AGIAGI TechnologyBeyond Earth Orbit
Page 3 and 4: Introduction (Woodburn)• Welcome
Page 5 and 6: Current/Historical Missions (Hall)
Page 7 and 8: Recent enhancements to Astrogator(B
Page 9 and 10: Orbit determination (Woodburn)• C
Page 11 and 12: Sequential range• Ambiguous two w
Page 13 and 14: Trk-34 tracking data format• Very
Page 15 and 16: Lunar gravity process noise model
Page 17 and 18: LP Position UncertaintyPosition Unc
Page 19 and 20: Central Bodies (Coppola)• Celesti
Page 21 and 22: Central Bodies (cont’d)• CB use
Page 23 and 24: CB Mu Values• Orbital element con
Page 25 and 26: Default CB Ephemeris Settings• Su
Page 27 and 28: Modifying CB ephemeris• Ephemeris
Page 29 and 30: Default Moon Attitude• Interpolat
Page 31 and 32: Attitude Reference• "Report of th
Page 33 and 34: Eclipse and Obstruction (LOS)• ST
Page 35 and 36: LTD Issues• Graphics display True
Page 37: Interplanetary Propagation (Berry)

AGI Technology Beyond Earth Orbit

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