Real-time capable trajectory synthesis via multivariate interpolation methods for a moon landing manoeuvre

Conventional solutions to control design problems in complex space missions are often based on a solution of an associated optimal control problem. Due to limited onboard computing capacity, the computation of an optimal trajectory and a dedicated controller are commonly carried out offline, in adva...

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Veröffentlicht in:	CEAS space journal 2014-06, Vol.6 (2), p.107-118
Hauptverfasser:	Lockner, E., Oehlschlägel, T., Theil, S., Knauer, M., Tietjen, J., Büskens, C.
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerospace Technology and Astronautics Computation Design engineering Engineering Initial conditions Interpolation Lunar landing Mathematical models Onboard Optimization Original Paper
Online-Zugang:	Volltext
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