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飞行器稳定性导数的参数辨识
聂雪媛; 杨国伟
Source Publication2016海峡两岸流体力学研讨会论文摘要集
2016-09-04
Conference Name2016海峡两岸流体力学研讨会
Conference Date2016-09-04
Conference Place中国青海西宁
Abstract静、动态稳定性特性是在飞行器设计过程中关心的重要问题,它们是飞行器控制系统设计、操纵及稳定性分析的重要参数。飞行器在配平攻角处的静、动态稳定性参数决定了飞行器的运动形态,即飞行器能否稳定在配平攻角,如果不能稳定在配平攻角,它将演化至何种运动形态。
Keyword配平攻角 稳定性导数 飞行器控制系统 动态稳定性 运动形态 飞行器设计 参数辨识 稳定性分析 风洞实验 飞行试验
DepartmentLMFS流固耦合与数值计算(LHO)
Language中文
Document Type会议论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/60847
Collection流固耦合系统力学重点实验室
高温气体动力学国家重点实验室
Affiliation中国科学院力学研究所流固耦合系统力学重点实验室
Recommended Citation
GB/T 7714
聂雪媛,杨国伟. 飞行器稳定性导数的参数辨识[C],2016.
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