@inproceedings{oai:jaxa.repo.nii.ac.jp:00007353,
 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 present an efficient calibration technique for rhumb-line attitude control manoeuvres for spin-stabilized satellites. The only measurements used in the calibrations are the solar aspect angles generated by a common V-slit Sun sensor. Both the path-length and rhumb-line angle can be established accurately by using the initial and final Sun aspect angles of two independent manoeuvre paths. This technique was applied successfully for the CONTOUR mission in 2002 before executing a full 180-deg flip manoeuvre. The final attitude error at the end of the manoeuvre was below 3 degrees., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0064734048},
 pages = {295--302},
 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 = {Calibration Technique for Attitude Manoeuvres of Spinning Satellites},
 volume = {2009},
 year = {2010}
}