飞行系统的英文

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用"飞行系统"造句

flight system

飞行: flight; flying; av ...
系统: system
飞行系统公司: flight systems inc

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例句与用法

The flight ' s atmospheric dynamic characteristics is considered , the aircraft is modeled as a combination of objects . most compositions , such as scene system , flight system , flight ' s sound and control surface are all simulated
)等建模软件建立了相应的三维表现模型；模拟了飞机的主要系统：飞行系统、视景系统、仪表系统和音响系统。
Secondly , software engineering method is introduced to the course of deve - lopment of the platform , which is intended to solve some common problem occurred in development of flight control simulation system and standardize the process of analysis and coding
该控制功能框架实现了建模框架和仿真框架的分离。其次,针对飞行仿真系统开发中存在的问题,通过对飞行系统模型及仿真系统的具体分析,引入软件工程方法。
Here , the aircraft is in extreme flight conditions that is high angles of attack and high angular rates . it can encounter severe nonlinear effects . detailed descriptions of the flight dynamic , aerodynamic models , inverse dynamic and the choice of the control variable are given
2 、应用经典的微分几何方法研究了一般的飞行状态下飞机飞行的控制律，指出不利用矢量推力的飞行系统的控制方程一般都是可以逐步通过动态状态反馈，适当的坐标变换和正则静态反馈等三个步骤得以线性化。
A integrated flight / propulsion control ( ifpc ) theoretical schema was designed based on this concept and a engineering schema was developed after take consideration of currently engineering condition and the requirements of in - service aircraft upgrade . a auto - flight system was designed which can achieve accurate flight movement control and increase performance of flight task such as ascend , cruise , te
基于该概念设计了飞推综合原理方案，并在考虑工程实现条件及现役飞机改进、改型要求后建立了工程实现方案，设计了轨迹跟踪方式的自动飞行系统，解决了轨迹生成、表示、管理、跟踪等问题，能够实现运动状态的精确控制，提高爬升、巡航等任务的性能。
As to the modelling of integrated flight / propulsion system , this paper mainly investigated and the modelling methods of flight kinetics and propulsion system thermodynamics , building up the real - time models of body kinetics . then we integrated the component - level thermodynamics model of engine , solved the problem of matching of initial points in the integrated simulation of flight / engine and the interactive parts of flight system and propulsion system
对于综合飞行/推进系统建模,本文主要研究的是飞行动力学和推进系统热力学的建模方法,建立了飞机动力学实时仿真模型。并结合前人已建立的发动机部件级热力学模型,本课题在解决了飞机/发动机综合仿真中的起始点匹配问题的基础上,完成飞行系统和推进系统的交互部分,最终建立飞行/发动机综合实时仿真模型。