Optimal Linear Attitude Estimator

An optimal linear attitude estimator is presented for the case of a single-point real-time estimation of spacecraft attitude using the minimum-element attitude parameterization: Rodrigues (or Gibbs) vector g. The optimality criterion, which does not coincide with Wahba's constrained criterion,...

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Veröffentlicht in:	Journal of guidance, control, and dynamics control, and dynamics, 2007-11, Vol.30 (6), p.1619-1627
Hauptverfasser:	Mortari, Daniele, Markley, F. Landis, Singla, Puneet
Format:	Artikel
Sprache:	eng
Schlagworte:	Accuracy Aerospace engineering Algorithms Applied sciences Computer science control theory systems Control theory. Systems Exact sciences and technology Modelling and identification
Online-Zugang:	Volltext
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