@inproceedings{oai:jaxa.repo.nii.ac.jp:00007356,
 author = {van, der Ha  Jozef C.},
 book = {アストロダイナミクスシンポジウム講演後刷り集, Proceedings of 19th workshop on JAXA Astrodynamics and Flight Mechanics},
 month = {Mar},
 note = {アストロダイナミクスシンポジウム (2009年7月30-31日. 宇宙航空研究開発機構宇宙科学研究本部)), Workshop on JAXA Astrodynamics and Flight Mechanics, 2009 (July 30-31, 2009. Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan, The paper presents the Kalman Filter (KF) adaptation of the Tanygin-Shuster (T-S) weighted least-squares algorithm for spin-axis attitude determination. This KF method is suitable for sequential real-time applications. The iteration procedure which led to the unit-vector normalization in the least-squares version of the T-S algorithm has been modified for the sequential approach presented here. This iteration is beneficial for the stability of the attitude determination results. The benefit of the unit-vector normalization has been demonstrated on the basis of real sensor data from the CONTOUR satellite., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0064734051},
 pages = {314--321},
 publisher = {宇宙航空研究開発機構宇宙科学研究本部, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)},
 title = {KALMAN FILTER FOR SPIN-AXIS ATTITUDE ESTIMATION},
 volume = {2009},
 year = {2010}
}