2010
DOI: 10.1016/j.actaastro.2009.06.013
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The first Rosetta asteroid flyby

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Cited by 24 publications
(8 citation statements)
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“…The mentioned 5% margins allocated for each DSM is compliant with ESA margin philosophy for science assessment studies (ESA, 2014). It should also be noted that TCMs for the Rosetta fly-bys of (2867) Steins and (27) Lutetia were both well below 1 m s -1 (Accomazzo et al, 2010(Accomazzo et al, , 2012 as a guide to the margin requirement. Figure 9 shows the spacecraft in its deployed and launch configuration respectively.…”
Section: Mission Analysismentioning
confidence: 99%
“…The mentioned 5% margins allocated for each DSM is compliant with ESA margin philosophy for science assessment studies (ESA, 2014). It should also be noted that TCMs for the Rosetta fly-bys of (2867) Steins and (27) Lutetia were both well below 1 m s -1 (Accomazzo et al, 2010(Accomazzo et al, , 2012 as a guide to the margin requirement. Figure 9 shows the spacecraft in its deployed and launch configuration respectively.…”
Section: Mission Analysismentioning
confidence: 99%
“…27 shows the distribution of true flyby distances for each asteroid mass, when noise terms are added to the initial condition with standard deviations on position and velocity components of r ¼ 5 km and r ¼ 10 cm/s respectively as order-of-magnitude estimates of the possible uncertainty of the state elements relative to the asteroid from the guidance, navigation and control subsystem. These estimates were obtained by looking at past missions and concepts for deep space navigation relative to asteroids (Ozaki et al, 2016) (Accomazzo et al, 2010) (Hashimoto et al, 2010) (Cui and Zhu, 2014). Fig.…”
Section: Sensitivity To Initial Conditions and Asteroid Massmentioning
confidence: 99%
“…Seven years of active cruise, in which several planet gravity assist swing-bys and two asteroid fly-bys were carried out [4][5][6][7][8][9][10], were followed by the final part of the cruise, where Rosetta ( Fig. 1-Note: manoeuvres are not necessarily represented as actually done in flight, rather as a single event and with the size resulting from a specific trajectory optimisation run) had to fly at distances from the Sun that had never been reached before by a solarpowered spacecraft (aphelion was reached on 3 October 2012 at about 5.3 AU distance) [11].…”
Section: Years and Tomentioning
confidence: 99%