Browse > Article
http://dx.doi.org/10.5139/JKSAS.2006.34.2.036

Investigation of Dual-Spin Turn and Attitude Acquisition of Satellite  

Seo, Hyeon-Ho (한국항공우주연구원)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.34, no.2, 2006 , pp. 36-47 More about this Journal
Abstract
The process of dual spin turn maneuver is introduced for attitude acquisition or recovery from flat spin state of a satellite. The physical principle of momentum transfer during dual spin turn is explained clearly. The case studies of special dual spin turn, in addition to the conventional dual spin turn, that are known as an acceptable cases, are performed to investigate the principle of dual spin turn and to provide a physical insight as well as the solution of dual spin turn. This study is done based on case-study simulation, which includes two-state control scheme composed of open-loop maneuver and energy dissipation device. Furthermore, we investigate the stability for the verification of all control cases after implementing two-stage control. We also provide the simulation scenario of flat spin recovery using dual spin turn method as an example.
Keywords
Dual Spin Turn, Momentum Transfer; Passive Damper; Momentum; Bias Satellite; Attitude Acquisition Maneuver; Flat Spin Recovery;
Citations & Related Records
연도 인용수 순위
  • Reference
1 서현호, 이승우, '시뮬레이션을 통한 위성의 Dual-Spin Turn 개선방법 연구', 한국항공우주학회 추계학술발표회, pp. 172-176, 2004
2 Sidi, M. J., 'Spacecraft Dynamics and Control : A Practical Engineering Approach', Cambridge Univ., Chap.d
3 Guelman, M., 'On Gyrostat Dynamics and Recovery', Journal of the Astronautical Sciences, Vol. 32, No.2, Apr-Jun, 1989, pp. 109-119
4 Barba, P. M., Aubrun, J. N., 'Satellite Attitude Acquisition by Momentum Transfer', AIAA Journal, Vo1.14, No.10, 1976, pp.1382 -1386   DOI   ScienceOn
5 Barba, P. M., Furumoto, N., Leliakov, I. P., 'Techniques for flat-spin recovery of spinning satellites', AIAA-1973-859, Aug. 1973
6 Hubert, C., 'Dynamics of the Generalized Dual Spin Turn', RCA Review, Vol. 41, Sep. 1980, pp. 449-471
7 Junkins, J. L., 'Optimal Spacecraft Rotational Maneuvers', Elsevier, Amsterdam, 1986, pp. 114-132
8 Kaplan, M. H., 'Modern Spacecraft Dynamics and Control', Wiley, New York, 1976, Chap.9
9 Bang, H., Kim, S. and Hwangbo, H., 'Feedback Control Law Design for the Dual Spin Turn of Spacecraft', Journal of Guidance and Control, Vol. 20, No.3, May.-Jun. 1997, pp. 450-456   DOI   ScienceOn
10 Kaplan, M. H., Patterson, T. C., Ramos, A., 'Attitude Acquisition Maneuver for A Bias Momentum Spacecraft', US Patent, Dec. 22, 1981
11 Ogata, K, 'System Dynamics', 3rd Ed., Prentice Hall, pp. 64-65
12 Gebman, J. R., Mingori, D. L., 'Perturbation Solution for the Flat Spin Recovery of a Dual-Spin Spacecraft', AIAA Journal, Vo1.14, No.7, 1976, pp. 859-867   DOI   ScienceOn
13 Hubert, C., 'Spacecraft Attitude Acquisition from an Arbitrary Spinning or Tumbling State', Journal of Guidance and Control, Vol. 4, Mar-Apr. 1981, pp. 164-170   DOI