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为了对舰载飞机着舰下滑时的跃升操纵策略进行研究,建立了飞机飞行动力学模型和驾驶员模型。在此基础上,根据“50 ft跃升规范”要求,以F/A-18舰载飞机为例,运用MATLAB/SIMULINK软件,对采取不同操纵策略下的飞机跃升飞行历程进行了仿真分析。结果表明,F/A-18舰载飞机在着舰下滑状态下无法达到“50 ft跃升规范”。此外,飞机在不开启动力补偿的情况下,飞行员需同时操纵油门杆和驾驶杆来实现轨迹跃升。
In order to study the strategy of leaping maneuver when the carrier-based aircraft glides down, the aircraft flight dynamics model and driver model are established. On the basis of this, based on the requirements of “50 ft jerk”, taking the F / A-18 carrier-based aircraft as an example, this paper uses MATLAB / SIMULINK software to simulate and analyze the flight jumper flight under different maneuver strategies. The results show that the F / A-18 carrier-based aircraft can not reach the “50 ft jumpers” under the condition of landing warships. In addition, the aircraft does not open the case of power compensation, the pilot must simultaneously control the throttle lever and the steering rod to achieve trajectory jumped.