Comparison of different methods to compute a preliminary orbit of Space Debris using radar observations

We advertise a new method of preliminary orbit determination for space debris using radar observations, which we call Infang†. We can perform a linkage of two sets of four observations collected at close times. The context is characterized by the accuracy of the range ρ, whereas the right ascension...

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Veröffentlicht in:	Proceedings of the International Astronomical Union 2014-07, Vol.9 (S310), p.154-155
Hauptverfasser:	Ma, Hélène, Gronchi, Giovanni F.
Format:	Artikel
Sprache:	eng
Schlagworte:	Astronomical instruments Astronomy Contributed Papers Declination Errors Integrals Linkages Mechanics Orbits Radar Space debris Stars & galaxies
Online-Zugang:	Volltext
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