Detail Optimal Attitude Stabilization of Spacecraft Using Minimal Kinematic Parameters   Oleh:  Park, Yonmook ; Tahk, Min-Jea Jenis: Article from Article Dalam koleksi: Final Program and Book of Abstracts: The 4th Asian Control Conference, September 25-27, 2002 (Sep. 2002), page 881-885. Topik: Minimal Kinematic; Cayley-Rodrigues Parameters; Fulltext: AC021515.PDF (369.14KB) Isi artikel In a recent study, we have presented a robust control scheme for the three-axis attitude stabilization of rigid spacecraft with inertia uncertainties. In the present paper, the previous robust control scheme is extended to the nonlinear optimal attitude control of rigid spacecraft. The attitude motion of rigid spacecraft described in terms of either the Cayley-Rodrigues parameters or the Modified Rodrigues parameters is considered. A numerical example is given to illustrate the theoretical results presented in this paper. Opini Anda Klik untuk menuliskan opini Anda tentang koleksi ini! Kembali

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