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Attitude control of a flexible satellite in noisy environment

Attitude control of a flexible satellite in noisy environment

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A method is presented for the design of a discrete, state-vector feedback controller operating on an open-loop unstable process. Kalman filtering is used for state estimation and the effectiveness of this technique is evaluated for high levels of noise.

References

    1. 1)
      • R.J. Fitzgerald . Divergence of the Kalman filter. IEEE Trans. , 736 - 747
    2. 2)
      • F.A. Leckie , G.M. Lindberg . The effect of lumped parameters on beam frequencies. Aeronaut. Q. , 3 , 224 - 240
    3. 3)
      • Longbottom, G.: `Dynamic modelling of structural frames', 1973, M.Phil. thesis, University of Leeds.
    4. 4)
      • J.S. Archer . Consistent mass matrix for distributed systems. Proc. Am. Soc. Civ. Eng. , 2 , 161 - 178
    5. 5)
      • N.O. Myklestad . A new method of calculating natural modes of uncoupled bending vibration of airplane wings and other types of beams. J. Aeronaut. Sci. , 153 - 162
    6. 6)
      • D. Smart , K.F. Gill , J.H. Gething , J.A. Holt . Dynamic analysis of flexible space vehicles having uncoupled control axes. Aeronaut. J. , 560 - 569
    7. 7)
      • R.A. Smith . Matrix equation XA + BX = C. SIAM J. Appl. Math. , 198 - 200
    8. 8)
      • R.E. Kalman , R.S. Bucy . New results in linear filtering and prediction theory. Trans. ASME J. Basic Eng. , 95 - 108
    9. 9)
      • Gething, J.M.: `Attitude control of a momentum stabilised communication satellite having large flexible appendages', 1973, Ph.D. thesis, University of Leeds.
    10. 10)
      • E.C. Pestel , F.A. Leckie . (1963) , Matrix methods in elastomechanics.
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