SDS-4 Attitude Control System: In-Flight Results of Three Axis Attitude Control for Small Satellites

التفاصيل البيبلوغرافية
العنوان: SDS-4 Attitude Control System: In-Flight Results of Three Axis Attitude Control for Small Satellites
المؤلفون: Yuta Nakajima, Takashi Ohtani, Keiichi Hirako, Naomi Murakami, Yosuke Nakamura, Koichi Inoue
المصدر: IFAC Proceedings Volumes. 46:283-288
بيانات النشر: Elsevier BV, 2013.
سنة النشر: 2013
مصطلحات موضوعية: Attitude control, Attitude control system, Engineering, Automatic Identification System, Spacecraft, business.industry, law, Satellite, General Medicine, Aerospace engineering, business, Simulation, law.invention
الوصف: The Small Demonstration Satellite (SDS) program is a JAXA technology demonstration program, targeting the in-orbit demonstration of advanced technologies using small satellites. Following the success of SDS-1, the SDS-4 spacecraft was successfully launched on 18 May 2012 and continues the in-flight demonstration of a space-based Automatic Identification System (AIS) as well as numerous flight experiments. This paper describes the in-flight results of the Attitude Control System (ACS) for 50kg class small satellites using 3-axis zero-momentum stabilization.
تدمد: 1474-6670
الوصول الحر: https://explore.openaire.eu/search/publication?articleId=doi_________::ffbd3fd6fbff65ffd86f3e7e564d7d36Test
https://doi.org/10.3182/20130902-5-de-2040.00077Test
حقوق: CLOSED
رقم الانضمام: edsair.doi...........ffbd3fd6fbff65ffd86f3e7e564d7d36
قاعدة البيانات: OpenAIRE