摘要
针对设计的飞机拦阻系统 ,在对其液压系统及拦阻期间运动学、静力学、动力学分析的基础上 ,建立起飞机拦阻系统的数学模型 ,并以MATLAB为仿真软件 ,用仿真方法对拦阻期间的受控参数如飞机过载、拦阻钢缆的拉力、拦停距离等的变化规律进行了分析研究 ,确切模拟了飞机拦阻系统的工作过程 ,对飞机拦阻系统的拦阻性能作了全面的定量分析 ,对改进和改善我国大多数机场的应急着陆设施有着重要意义。
In this paper,based on the complex analyses of hydraulic system, kinematics, statics and dynamics of system, mathematical model of the designed aircraft arresting system was built, and using simulation method analyse and study the arresting performances. Simulation software was MATLAB. Simulation could imitate the working process of the system. The design of this system had an important meaning in reforming and improving the landing emergency facilities in most of airports of our country.
出处
《航空计算技术》
2002年第3期34-37,共4页
Aeronautical Computing Technique
