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turbojet engine model 涡喷发动机模型
A turbojet engine used todrive an external propeller. 涡轮螺旋桨发动机一种用于推动外部螺旋桨的涡轮喷气式发动机。
A turbojet engine used to drive an external propeller. 涡轮螺旋桨发动机一种用于推动外部螺旋桨的涡轮喷气式发动机
A model for 100N class micro turbojet engine is established.Software and hardware system design of the controller is accomplished by using robust control algorithm. 建立了100N推力级微小型涡喷发动机模型,应用鲁棒控制算法进行了控制器软、硬件系统开发设计;
The validation of method is demonstrated by one-spool turbojet engine. 单轴涡喷发动机的算例证明了方法的有效性。
The particle trajectory is calculated with certain amoune of selected control rules by establishing mathematical mod els such as whole missile mass calculation model,aerodynamic estimation model and turbojet engine performance interpolation. 通过建立全弹质量计算模型、气动估算模型和涡喷发动机性能插算等数学模型 ;选取一定的控制规律进行了质点弹道计算 .
As an example,the method provided was adopted to rectify the parameters in the simulation model of a given twin-spool reheated turbojet engine,and the simulation achieved satisfactory accuracy. 应用本文方法对某型双转子加力涡喷发动机仿真模型进行校正，获得了满意的仿真精度。
A turbojet engine in which a fan supplements the total thrust by forcing air directly into the hot turbine exhaust. 涡轮风扇喷气发动机一种涡轮喷气发动机带有一个风扇，通过将空气直接压入热的涡轮排气管而补充总推力
Model based AFR control strategy requires accurate engine model first. 基于模型的空燃比控制策略首先要求有精确的模型，均值模型是非线性模型，其精度高、表达形式简单，能够满足控制过程实时性的要求，是比较理想的模型。
Breathing can be divided into jet engine turbojet engine, turbo-fan jet engine and combustion ramjet engine. 如果按照这一定义，除远程巡航导弹外，各种飞航式反舰导弹和空地、空舰飞航式导弹也属于巡航导弹。
Chiang, H. D., and W. C. Ho, “Miniature Liquid Fueled Turbojet Engine”, U. S. Patent #5782079. 蒋小伟，何无忌，“超小型燃油气涡轮喷射引擎”中华民国第136677号专利。
Smetana, F. O.,“Turbojet Engine Gas Path Analysis A Review,”AGARD Conference Proceedings, No. 165, 4-5 April, 1974. 陈大光;张赫然;“用气动热力参数对发动机故障进行诊断与定位的实用方法;”北京航空航天大学硕士论文第二章;1989年.
With a reuse engineering model it occurs one project at a time. 对于重用工程模型,一个项目要进行一次域分析。
The rocket sled test was carried out for overall investigating the dynamic process of missile turbojet engine starting and accelerating. 为了研究弹用涡轮喷气发动机动态启动加速过程,开展了发动机火箭橇试验研究。
The rocket sled test can imitate the dynamic conditions of missile launching, it is very important for missile turbojet engine design. 火箭橇试验能够真实的模拟导弹发射条件,它对于弹用涡轮喷气发动机研究具有十分重要的意义。
The effect of prior knowledge on convergence of engine model and the Bayesian updating of a quadratic linear model are also analyzed. 分析了发动机先验知识对模型收敛的影响及二阶线性模型的贝叶斯更新。
The rocket sled test was carried out for overall investigatingthe dynamic process of missile turbojet engine starting and accelerating. 为了研究弹用涡轮喷气发动机动态启动加速过程，开展了发动机火箭橇试验研究。
J. P. Wang and Y. F. Liu: Theoretical Analysis on Simplified Pulse Detonation Engine Model, Shock Waves (Accepted). 王健平、刘云峰、李廷文:脉冲爆轰发动机预爆轰点火的数值模拟;空气动力学报;2004;22(4);475-480.
The model can be used for engine control system exploiter and ECU calibration with engine model. 该模型可以与发动机模型一起用于发动机电控系统的开发。
As an example,a robust control law is designed to the twin-spool turbojet engine system using the given method.The result shows that the given method is feasible. 文中以双转子涡喷发动机控制器设计为例,设计了基于LMI的鲁棒控制器,结果表明所给方法是可行的。