舰载飞机着舰拦阻动力学分析  

Arresting Dynamics Research of Carrier Aircraft

作　　者：胡孟权[1] 林国华[1] 

机构地区：[1]空军工程大学工程学院,陕西西安710038

出　　处：《空军工程大学学报（自然科学版）》2000年第5期8-11,共4页Journal of Air Force Engineering University(Natural Science Edition)

摘　　要：提出了舰载飞机非对称、偏心着舰时拦阻力的计算方法 ,考虑了拦阻挂钩可在拦阻索上滑动的情况 ,建立了舰载飞机着舰动力学模型。进行了舰载飞机着舰拦阻仿真和分析研究 ,分析了着舰偏心距、非对称性对飞机着舰的影响。The article puts forward a method for calculating the arresting force of carrier aircraft in the case the aircraft meets the cable off center and the aircraft motion is unsymmetrical. The condition under which the hook will or will not slip on the cable is considered. Based on a great deal of numerical results, the article analyzed the impact of unsymmetrical motion and off center on landing dynamics of carrier aircraft.

关 键 词：舰载飞机 偏心 拦阻 

分 类 号：V212.13[航空宇航科学与技术—航空宇航推进理论与工程]