| 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)
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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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