39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2003
DOI: 10.2514/6.2003-4802
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Approach Navigation for a Titan Aerocapture Orbiter

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Cited by 13 publications
(5 citation statements)
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“…Improvements in Titan's ephemeris based on ground-based observations coupled with Titan ephemeris data gleaned from Cassini's planned 44 flybys of Titan will result in one to two orders of magnitude improvement in the Titan ephemeris knowledge, thus significantly reducing that error component (ref. 42). Early in the Titan approach phase, uncertainties in the spacecraft state dominate the errors.…”
Section: Navigation Systemsmentioning
confidence: 99%
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“…Improvements in Titan's ephemeris based on ground-based observations coupled with Titan ephemeris data gleaned from Cassini's planned 44 flybys of Titan will result in one to two orders of magnitude improvement in the Titan ephemeris knowledge, thus significantly reducing that error component (ref. 42). Early in the Titan approach phase, uncertainties in the spacecraft state dominate the errors.…”
Section: Navigation Systemsmentioning
confidence: 99%
“…The orbit determination uncertainties include the reaction caused by the probe release mechanism and the reaction caused by the release of the orbiter truss, as well as data errors (ref. 42). Uncertainty in the ephemeris of Titan provide a large initial contributor to the navigation uncertainty.…”
Section: Navigation Systemsmentioning
confidence: 99%
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