Volume 29 Issue 1
Jan.  2003
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Zhang Ping, Wang Dong, Chen Zongjiet al. PostStall Maneuver Control Law for Aircrafts with New Control Configuration[J]. Journal of Beijing University of Aeronautics and Astronautics, 2003, 29(1): 23-26. (in Chinese)
Citation: Zhang Ping, Wang Dong, Chen Zongjiet al. PostStall Maneuver Control Law for Aircrafts with New Control Configuration[J]. Journal of Beijing University of Aeronautics and Astronautics, 2003, 29(1): 23-26. (in Chinese)

PostStall Maneuver Control Law for Aircrafts with New Control Configuration

  • Received Date: 06 Jul 2001
  • Publish Date: 31 Jan 2003
  • A post-stall maneuver control law for aircraft with new control surfaces and trust vectoring control is proposed. The air dynamical data table is operated by minimal mean-square value of the error between the air data and the combined continued functions. The 6 freedom nonlinear dynamical equations of the aircraft are predigested at static operating points by extended linearization which still possess nonlinear characters. The control laws of the inner closed-loop system and post-stall maneuver are obtained through using symbol operations design. Simulation result shows that the control law is effective for the post-stall maneuver design of modern aircrafts.

     

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