Achieving spacecraft rapid rotation using minimally redundant coplanar gyrodyne system
|1Yefymenko, MV, 2Lutsenko, HV, 2Paromova, TO |
1«Hartron-UKOM» scientific manufacturing company, Limited Liability Company, Zaporizhia, Ukraine
2National Technical University, Zaporizhia, Ukraine
|Kosm. nauka tehnol. 2015, 21 ;(5):48–56|
|Section: Spacecraft dynamics and control|
|Publication Language: Russian|
The subject of this article is to consider a minimally redundant coplanar gyrodyne structure for the spatial reorientation of the spacecraft. The proposed orientation algorithm provides a required reorientation of the spacecraft and optimal gyrodyne configuration. The results of the computer modeling of proposed algorithm are shown.
|Keywords: attitude control, gyrodyne, spacecraft|
1. Jermolenko Je.O., Vorotnikov V.A. Structural and logical model of a primary analysis of rocketry market attractiveness [Strukturno-logichna model' pervynnogo analizu rivnja pryvablyvosti rynkiv raketno-kosmichnoi' tehniky]. Visnyk social'no-ekonomichnyh doslidzhen': Zb. nauk.prac', Is.4(51), P.66—75 (2013) [in Ukrainian].
2. Satellite Manufacturing and Launch Services: 3rd Ed. Northern Sky Research Report, 17 p. (USA, 2013).
3. Satellites to be Built &Launched by 2021: A Euroconsalt Research Report. Euroconsalt. 224 p. (France,2011).