摘要
利用MATLAB仿真技术构建某型无人机的空滑迫降模型,借助该模型仿真计算无人机空滑迫降过程,分析在空滑盘旋和空滑下降两个迫降飞行阶段中各项因素对空滑迫降能力的影响。仿真计算结果表明,设置合适的参数有利于实现无人机空滑迫降范围最大化,同时结合实际大气环境中风的影响,提出了不同的空滑能量区域划分。该研究方法可有效评估无人机的空滑迫降能力。
Based on MATLAB simulation technology,a forced landing model without power is established for a certain aircraft.With the help of this flight simulation model,the process of forced landing can be simulated,the influence associated with various factors on the ability of forced landing during the unpowered hover and glide can also be analyzed.The results of simulation calculation indicate that setting proper parameters can be beneficial to maximize the range of forced landing.Meanwhile,considering the influence of wind in the actual atmospheric environment,different divisions of energy range of forced landing are proposed.The research method can effectively estimate the ability of forced landing without power.
作者
韩锐
谢欢
潘怡衡
李锐
李涛
HAN Rui;XIE Huan;PAN Yi-heng;LI Rui;LI Tao(Technical Center,Chengdu Aircraft Industrial(Group)Co.,Ltd.,Chengdu 610073,China)
出处
《飞行力学》
CSCD
北大核心
2019年第2期87-91,共5页
Flight Dynamics
关键词
空滑迫降
空滑漏斗
空滑能量区域
飞行仿真
能力评估
forced landing without power
funnel of forced landing
energy range of forced landing
flight simulation
capability assessment