An Attitude Determination Algorithm for a Spacecraft Using Nonlinear Filter

In this paper, the algorithm for a real time attitude estimation of a spacecraft motion is investigated. The proposed algorithm for attitude estimation is the second order nonlinear filter form not containing truncation error in estimation values. The proposed second order nonlinear filter has impro...

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Veröffentlicht in:Journal of mechanical science and technology 1999-02, Vol.13 (2), p.130-143
Hauptverfasser: Yoon, Yong Joong, Choi, Jae Weon, Lee, Jang Gyu, Fang, Tae Hyun
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Sprache:eng
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