본문 바로가기
HOME> 논문 > 논문 검색상세

논문 상세정보

Journal of mechanical science and technology v.24 no.6, 2010년, pp.1319 - 1327   SCIE
본 등재정보는 저널의 등재정보를 참고하여 보여주는 베타서비스로 정확한 논문의 등재여부는 등재기관에 확인하시기 바랍니다.

An accurate and simple model for flexible satellites for three-dimensional studies

Shahriari, Shahram    (Department of Mechanical Engineering, Tarbiat Modares University   ); Azadi, Shahram    (Faculty of Mechanical Engineering, K. N. Toosi University of Technology   ); Moghaddanr, Majid M.    (Faculty of Mechanical Engineering, Tarbiat Modares University  );
  • 초록

    In this paper, an accurate and simple model of a satellite with two flexible solar panels for three-dimensional dynamic studies is proposed and compared with other models. In the proposed model, each solar panel is assumed to be rigid and attached to the satellite body via a simple hinge, a torsional spring, and a torsional damper. Kane's method is utilized to derive the equations of motion. The model of flexible satellite with the assumption of Euler-Bernoulli beam for the solar panels, generally used in the literature, has been introduced for comparison. A comprehensive model of flexible satellite, considering solar panels as flexible and finite element panels, has been provided in ADAMS environment as a reference when comparing the two mentioned models. The Euler-Bernoulli model does not appropriately simulate-the three-dimensional motion of satellite. Conversely, the hinged, rigid-panel model proposed in this paper provides suitable results in both two- and three-dimensional maneuvers.


  • 주제어

    Satellite .   Dynamic modeling .   Flexibility .   Kane's method .   Solar panels.  

  • 참고문헌 (15)

    1. Y. Zeng, A. D. Araujo and S. N. Singh, Output feedback variable structure adaptive control of flexible spacecraft, Acta Astronautica. 44 (1)(1999) 11-22. 
    2. H. Bang, Y. Cho and H. Lee, Slewing maneuver control of flexible spacecraft by output feedback, Acta Astronautica, 55 (2004) 903-916. 
    3. Q. Hu and G. Ma, Variable structure control and active vibration suppression of flexible spacecraft during attitude maneuver, Aerospace Science and Technology, 9 (2005) 307-317. 
    4. Q. Hu and Y. Liu, A hybrid scheme of feed-forward/feed-back control for vibration suppression of flexible spacecraft with on-of actuators during attitude maneuver, International Journal of Information technology, 11 (12) (2005) 95-107. 
    5. B. N. Agrawal, R. S. Mcclelland and G. Song,, Attitude control of flexible spacecraft using pulse-width pulse-frequency modulation thrusters, Space Technology, 17 (1) (1997) 15-34. 
    6. G. Song and B. N. Agrawal, Vibration suppression of flexible spacecraft during attitude control, Acta Astronautica, 49 (2) (2001) 73-83. 
    7. Y. Chida, H. Soga, Y. Yamaguchi, T. Kida, I. Yamaguchi and T. Sekiguchi, On-orbit attitude control experiment using ETSVI by $H{\infty}$ control and two-degree-of-freedom control, Control Engineering Practice, 6 (1998) 1109-1116. 
    8. D. Gorinevsky and G. Vukovich, Control of flexible spacecraft using nonlinear approximation of input shape dependence on reorientation maneuver parameters, Control Engineering Practice, 5 (12) (1997) 1661-1671. 
    9. J. Zheng, S. P. Banks and H. Alleyne, Optimal attitude control of three-axis stabilized flexible spacecraft, Acta Astronautica, 56 (2005) 519-528. 
    10. H. Bang, C. Ha and J. H. Kim, Flexible Spacecraft attitude maneuver by application of sliding mode control, Acta Astronautica, 57 (2005) 841-850. 
    11. S. Parman and H. Koguchi, Controlling the attitude maneuvers of flexible spacecraft by using time-optimallfuel-efficient shaped inputs, Journal of Sound and Vibration, 221 (4) (1999) 545-565. 
    12. A. D. Meglio and A. Ercolifrnzi, Minimum time control of flexible spacecraft by Hamilton's principle, Meccanica, 32 (1997) 555-565. 
    13. T. R. Kane, P. W. Likins and D. A. Levinson, Spacecraft Dynamics, McGraw-Hill, (1981). 
    14. H. Baruh, Analytical dynamics, McGraw-Hill, Singapore, (1999). 
    15. K. A. Ford and C. D. Hall, Reorienations of spacecraft using momentum exchange devices, Ph.D. Dissertation, air force inst of tech. Wright-Patterson AFB (1997). 

 활용도 분석

  • 상세보기

    amChart 영역
  • 원문보기

    amChart 영역

원문보기

무료다운로드
  • 원문이 없습니다.
유료다운로드

유료 다운로드의 경우 해당 사이트의 정책에 따라 신규 회원가입, 로그인, 유료 구매 등이 필요할 수 있습니다. 해당 사이트에서 발생하는 귀하의 모든 정보활동은 NDSL의 서비스 정책과 무관합니다.

원문복사신청을 하시면, 일부 해외 인쇄학술지의 경우 외국학술지지원센터(FRIC)에서
무료 원문복사 서비스를 제공합니다.

NDSL에서는 해당 원문을 복사서비스하고 있습니다. 위의 원문복사신청 또는 장바구니 담기를 통하여 원문복사서비스 이용이 가능합니다.

이 논문과 함께 출판된 논문 + 더보기