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

WU Wenhai; SONG Liting; ZHANG Yang; WANG Jie; GAO Li

doi:10.13700/j.bh.1001-5965.2018.0481

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)

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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

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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

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.
- carrier aircraft,
- catapult take-off,
- crosswind disturbance,
- dynamic inverse,
- flight control

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References(24)

References

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