摘要
为研究舰载机在下滑着舰时飞行员的操纵策略,建立了着舰任务下的双通道飞行员模型。以人工着舰时飞行员控制飞机进行轨迹跟踪为背景,以着舰时惯用的"反区"操纵技术为依据,确立了舰载机飞行员控制律,并对控制增益参数进行了自适应设计。最后结合F-18A舰载机,运用SIMILINK软件进行了仿真。结果表明,该模型能很好地反映着舰任务下的飞行员操纵特性,可为飞行员着舰操纵提供参考。
To study the pilot control strategy in carrier landing,a double-channels pilot model for carrier landing task is established. The pilot control law is established based on the "backside"control technique which is used to realize path tracking with the manual controlled carrier landing as the background,and the gain parameter of the pilot model are adaptively designed. Simulation validation is finally processed with the SIMILINK software combined with F-18 A aircraft. The result shows that the pilot model can reflect the pilot control characteristics and provide references to pilots for carrier landing.
出处
《飞行力学》
CSCD
北大核心
2016年第1期14-17,共4页
Flight Dynamics