飞机设计
飛機設計
비궤설계
AIRCRAFT DESIGN
2011年
6期
1-5,15
,共6页
舰载机%拦阻着舰%能量法%计算机仿真
艦載機%攔阻著艦%能量法%計算機倣真
함재궤%란조착함%능량법%계산궤방진
carrier-based aircraft%arrested landing%energy method%computational simulation
针对舰载机拦阻着舰过程，采用能量法分析了任意着舰姿态和位置下的拦阻力响应，建立了全机六自由度动力学模型，考虑了航母甲板风的影响以及航母纵摇和升沉运动。通过MATLAB／SIMULINK建立数学模型，并以一种偏心非垂直着舰拦阻状态为算例进行了仿真分析。
針對艦載機攔阻著艦過程，採用能量法分析瞭任意著艦姿態和位置下的攔阻力響應，建立瞭全機六自由度動力學模型，攷慮瞭航母甲闆風的影響以及航母縱搖和升沉運動。通過MATLAB／SIMULINK建立數學模型，併以一種偏心非垂直著艦攔阻狀態為算例進行瞭倣真分析。
침대함재궤란조착함과정，채용능량법분석료임의착함자태화위치하적란조력향응，건립료전궤륙자유도동역학모형，고필료항모갑판풍적영향이급항모종요화승침운동。통과MATLAB／SIMULINK건립수학모형，병이일충편심비수직착함란조상태위산례진행료방진분석。
During the arrested landing process of carrier-based aircraft, the energy method is applied to analysis the performance of arresting force when aircraft is arrested at different initial posture and position, and the 6-DOF motion equations is built, also considering the carrier motions and deck wind. An example is studied under off-center and non-vertical condition based on mathematical model which is build by MATLAB/SIMULINK tool box.
