Adaptive tracking control using synthesized velocity from attitude measurements

نویسندگان

  • H. Wong
  • Marcio S. de Queiroz
  • Vikram Kapila
چکیده

The attitude tracking control problem of uncertain rigid spacecraft without angular velocity measurements is addressed in this paper. The adaptive control law, which incorporates a velocity-generating filter from attitude measurements, is shown to ensure the asymptotic convergence of the attitude and angular velocity tracking errors despite unknown spacecraft inertia. Simulation results are presented to illustrate the theoretical results.

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عنوان ژورنال:
  • Automatica

دوره 37  شماره 

صفحات  -

تاریخ انتشار 2001