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Volume 45 Issue 4
Apr.  2019
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Journal of Beijing University of Aeronautics and Astronautics  > 2019  >  45(4): 662-671.
WU Wenhai, SONG Liting, ZHANG Yang, et al. Analysis of factors affecting catapult take-off of carrier aircraft and design of lateral control law[J]. Journal of Beijing University of Aeronautics and Astronautics, 2019, 45(4): 662-671. doi: 10.13700/j.bh.1001-5965.2018.0481(in Chinese)
Citation: WU Wenhai, SONG Liting, ZHANG Yang, et al. Analysis of factors affecting catapult take-off of carrier aircraft and design of lateral control law[J]. Journal of Beijing University of Aeronautics and Astronautics, 2019, 45(4): 662-671. doi: 10.13700/j.bh.1001-5965.2018.0481(in Chinese)
shu

Analysis of factors affecting catapult take-off of carrier aircraft and design of lateral control law

doi: 10.13700/j.bh.1001-5965.2018.0481
  • 1.

    Control and Engineering Department, Qingdao Branch, Naval Aviation University, Qingdao 266041, China

  • 2.

    Trainer Simulation Training Center, Naval Aviation University, Huludao 125001, China

More Information
  • Corresponding author: WU Wenhai, E-mail: 441211638@qq.com
  • Received Date: 16 Aug 2018
  • Accepted Date: 15 Oct 2018
  • Publish Date: 20 Apr 2019
    Abstract

  • The various factors affecting the carrier aircraft catapult take-off safety are analyzed in detail. The nonlinear six-degree-of-freedom motion model of the aircraft in climbing phase is established. The effect of the rolling and yaw motion and crosswind on the catapult take-off characteristics is simulated and analyzed, and it is found that the main influences on the rolling and side-slip movement of the carrier aircraft after leaving the ship are the deck rolling motion and crosswind disturbance respectively. The nonlinear dynamic inverse control method is proposed to keep the nonlinear features of the model, make the result more precise, and realize the decoupling control of directional and lateral motion states. The simulation result indicates that the designed lateral control law can ensure that the rolling angle of the aircraft meets the safety criterion of not exceeding 5° within 3 seconds after leaving the ship and that there will be no obvious side-slip phenomenon due to crosswind disturbance, which can guarantee the safe take-off of carrier aircraft.

     

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