期刊论文详细信息
ETRI Journal
Analysis of the Antenna Pointing Instability of a Satellite in Spin-Stabilized Injection Mode
关键词: Analysis of the Antenna Pointing Instability of a Satellite in Spin-Stabilized Injection Mode;   
Others  :  1183921
DOI  :  10.4218/etrij.94.0194.0023
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【 摘 要 】

A new mathematical model to predict the beam pointing instability of a nonconservative two-body satellite system in spinning injection mode has been developed by using Newton-Euler and projection methods. Since the on-axis and null axis of the omni antenna with toroidal pattern beam form a right angle, wobbling of the antenna on-axis is measured by determining the Euler angles which represent the orientation of the satellite’s spin axis. Bacause of the complexity of the system which is a time varying, nonstationary, nonlinear dynamical system, a numerical method is used for the analysis. Computer simulation results present the effects of the mass distribution and internal mass motion on the antenna beam pointing.

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【 参考文献 】
  • [1]D. L. Mingori and Y. Yam, "Mutation instability of a spinning spacecraft with internal mass motion and axial thrust," AIAA Paper no. 86-2271, AIAAJA AS Astrodynamics Conference, Williamsburg, VA, Aug. 18-20, 1986.
  • [2]A. C. Or, "Rotor-pendulum model for the perigee assist module mutation anomaly," The Journal of Guidance, Control and Dynamics, vol. 15, no. 2, Mar. 1992, pp. 297-303.
  • [3]J. E. Cochran, Jr. and J. Y. Kang, "Nonlinear stability analysis of the attitude motion of a spin-stabilized upper stage," AAS Paper 91-190, AAS/AIAA Space flight Mechanics Meeting, Houston, TX, Feb. 11-13, 1991.
  • [4]J. Y. Kang and J. E. Cochran, Jr., "Further investigation of anomalous attitude motion of a spin-stabilized upper stage," AAS Paper 91-480, AASIAIAA Astrodynamics Specialist Conference, Durango, Colorado, Aug. 19-22, 1991.
  • [5]J. Y. Kang and S. 3. Chung, "Resonances in the attitude motion of a spin-stabilized spacecraft," Proceedings of the Asia-Pacific Workshop on Multilateral Cooperation in Space Technology and Applications, Beijing China, Nov. 30 - Dec. 5, 1992, pp. 233-247.
  • [6]J. Y. Kang, K. K. Shin and J. M. Kim, "The analysis of the attitude motion of a satellite spin-stabilized at apogee phase," Proceedings of the Fall Conference of the Korea Society for Aeronautical & Space Sciences, Seoul Korea, Nov. 14, 1992, pp. 293-301.
  • [7]N. H. Abramson(ed), "The dynamic behavior of liquids in moving containers with applications to space vehicle technology," NASA SP-iO6, 1966.
  • [8]W. T. Thomson. Introduction to Space Dynamics, New York: Dover Publications Inc., 1986, p. 38, pp. 113-116.
  • [9]M. H. Kaplan, Modern Spacecraft Dynamics and Control, New York: John Wiley & Sons. Inc., 1976, p. 13, pp. 50-57.
  • [10]P. C. Hughes, Spacecraft Attitude Dynamics. New York: John Wiley & Sons, Inc., 1986.
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