摘要
为了有效分析飞机起飞过程中,飞机突然遭遇微下击暴流情形下的飞行特性以及飞机起飞轨迹的变化规律,以Cessna-C310为例,结合JSBSim飞行动力学仿真系统,对其在以上特殊情况下进行仿真测试。仿真结果表明,不同的风场强度会使飞机起飞轨迹及受力情况不同程度的改变且飞机受垂直风的影响较明显,另外,对比测试出了该机型所能承受的最大风场强度。
In order to analyze the flight characteristics of the airplane in the case of microburst and research the change rule of the airplane taking off effectively,a microburst wind shear model is established. Taking Cessna-C310 as an exampled,combinewith JSBSim flight dynamics simulation system,the simulation test is carried out under the above special circumstances. Simulationresults show that,different strength of the wind farm will take off trajectory and the forces of change and the degree of influence ofthe aircraft by the vertical wind obvious. In addition,a comparison test of the model provide the maximum wind strength.
出处
《舰船电子工程》
2018年第2期83-86,共4页
Ship Electronic Engineering
基金
中国博士后科学基金项目(编号:No.2016M602962
No.2017T100797)资助
