助手标题
全文文献 工具书 数字 学术定义 翻译助手 学术趋势 更多
查询帮助
意见反馈
共[8]条 当前为第1条到8条
 

相关语句
landing simulation
    Aerocraft Recovery and Landing Simulation Software System
    航天器回收着陆仿真软件系统(ARLSSS)简介
    Research on Taking Off and Landing Simulation System of the Certain UAV
    某型号无人机起飞、着陆仿真系统研究
    A full-aircraft assembly model based on ADAMS/Aircraft is defined, which includes wheel subsystems, landing-gear subsystems, a brake subsystem, and an airframe subsystem, and performs full-aircraft landing simulation analyses (including aircraft landing and drop).
    2.基于ADAMS/Aircraft模块定义了一个由机身、起落架、刹车和机轮子系统构成的全机模型,并进行了整机着陆仿真分析(包括降落和落震两部分)。
    In order to study the flight characteristics and control rules in taking off and landing period better to promote flight safety of UAV in this stage, we started the study of take off and landing simulation system research of UAV based on a certain type of UAV. This system is very complex, involves system modeling and simulation, sensor, network, correspondence, computer animation, therefore this topic has only done one part of entire simulation system development.
    为更好地研究无人机在起飞、着陆阶段的飞行特性,控制规律,以保证无人机在这一阶段的飞行安全,我们以某型无人机为对象进行无人机的起飞、着陆仿真系统研究。 此系统很复杂,涉及系统建模仿真、传感器、网络、通信、计算机动画等内容,因此本课题只做了整个仿真系统研制的一部分工作。
    This article mainly contains three parts, first is the overall design of taking off and landing simulation system . The system overall construction and the function of each subsystem and the communication mode in system have been determined.
    本文的主要内容包括三个部分,首先是起飞、着陆仿真系统的整体设计,确定了系统的整体结构,组成系统的各个分系统的主要功能及各分系统之间的通信模式。
    Having the mathematical model of UAV in this stage is very important for design the taking off and landing simulation system.
    其次,要设计起飞、着陆仿真系统,首先要得到无人机在这一阶段的数学模型。
    Gliding and leveling are considered in longitudinal landing simulation study.
    其纵向着陆仿真研究,主要考虑下滑段和拉平段。
    It defines a full-aircraft assembly model based on ADAMS/Aircraft software, which includes wheel subsystems, landing-gear subsystems, a brake subsystem, and an airframe subsystem. It performs full-aircraft landing simulation analyses (including aircraft landing and drop).
    基于ADAMS/Aircraft模块定义了一个由机身、起落架、刹车和机轮子系统构成的全机模型,并进行了整机着陆仿真分析(包括降落和落震两部分)。
 

首页上一页1下一页尾页 

 
CNKI主页设CNKI翻译助手为主页 | 收藏CNKI翻译助手 | 广告服务 | 英文学术搜索
版权图标  2008 CNKI-中国知网
京ICP证040431号 互联网出版许可证 新出网证(京)字008号
北京市公安局海淀分局 备案号:110 1081725
版权图标 2008中国知网(cnki) 中国学术期刊(光盘版)电子杂志社