Volume 29 Issue 11
Nov.  2003
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Jiang Zaiming, Zhang Shuguang. Research on integrated flight/propulsion control design[J]. Journal of Beijing University of Aeronautics and Astronautics, 2003, 29(11): 1042-1046. (in Chinese)
Citation: Jiang Zaiming, Zhang Shuguang. Research on integrated flight/propulsion control design[J]. Journal of Beijing University of Aeronautics and Astronautics, 2003, 29(11): 1042-1046. (in Chinese)

Research on integrated flight/propulsion control design

  • Received Date: 09 Jul 2003
  • Publish Date: 30 Nov 2003
  • A decentralized approach was set up for integrated flight/propulsion control(IFPC) design. Based on the gliding slope and terrain-following(TF) missions, the structures of compensators were firstly determined. The linear quadratic optimization with output feedback method was applied to determine the zeros of the compensators and the feedback gains. The effects of coupling factors between the velocity and the altitude paths were analyzed. The results show that if the coupling factors and weighting matrix for choice of the zeros of the compensators and the feedback gains are properly used, good control schemes are available, and the linear quadratic optimization with output feedback for IFPC design is favorable.

     

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