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型飞行器
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  type aerocraft
     The Design and Realization of a Type Aerocraft Pitot-Static Pressure System
     某型飞行器全静压检测系统的设计实现
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  “型飞行器”译为未确定词的双语例句
     Mixed H_2/H_∞ robust control technique is employed to design controllers for a aircraft motion control system.
     利用混合H2/H∞鲁棒控制技术设计了某型飞行器运动控制系统。
短句来源
     Development and Application of a Flight Vehicle Automatic Testing System Based on VXI Bus
     基于VXI总线的某型飞行器自动测控系统研制与应用
短句来源
     Applying this paper's method to some spacecraft′s attitude control problem, simulation result shows that the approach is quite effective.
     将文中的方法应用于某型飞行器的姿态控制中 ,仿真结果表明控制效果良好
短句来源
     The (4.2 g) paraboloid craft with(10 mm) focus is spin-stabilized to(700 r/m) prior to launch.
     当转速达到700 r/m时,质量为4.2 g,焦距为10 mm的抛物面型飞行器在单脉冲输出能量为13 J,重复频率50 Hz的TEA CO2激光器的推进下,成功实现了重复频率脉冲激光推进竖直自由飞行演示。
短句来源
     Research on Composite Control of Mass/Thrust Vectoring for a Kind of Saucer-Like Air Vehicle
     一类碟型飞行器质量/推力矢量复合控制研究
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  相似匹配句对
     (2)C shape;
     C ;
短句来源
     (3)D shape.
     D
短句来源
     AERODYNAMIC COEFFICIENTS IDENTIFICATION FOR A AXIS-SYMMETRIC FLIGHT VEHICLE
     轴对称飞行器气动参数辨识研究
短句来源
     Study on Six-degree of Freedom Simulation of a Flying Vehicle
     某飞行器六自由度仿真研究
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     Flight Simulator
     飞行器模拟器
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In this oaper the hybrid simulation problem of the vehicle control system by using Z-80 micro computer and analog mini-computer was studied and the hybrid ismulation system was success fully realized. A valiable example given here is useful for realizing hybrid simulation of control system with microcomputer. The result obtained with simulation technigue can be considered as the referential data in the design of certain type of the vehicle. Thesimulation program can be executed rn dfferent forms, such as FORTRAN—Z-80...

In this oaper the hybrid simulation problem of the vehicle control system by using Z-80 micro computer and analog mini-computer was studied and the hybrid ismulation system was success fully realized. A valiable example given here is useful for realizing hybrid simulation of control system with microcomputer. The result obtained with simulation technigue can be considered as the referential data in the design of certain type of the vehicle. Thesimulation program can be executed rn dfferent forms, such as FORTRAN—Z-80 assembly or Z-80 assembly language. FORTRAN—Z-80 program was given.

本文讨论了使用Z-80微型计算机和小型模拟计算机对某型飞行器控制系统进行混合仿真研究的问题,并成功地实现了混合仿真系统。文中给出使用微型计算机进行控制系统仿真的一个有用实例,采用仿真技术所获得的结果可为某型飞行器研制工作提供参考数据,仿真程序可以不同形式执行,如FORTRAN—Z-80汇编或Z-80汇编语言,本中给出FORTRAN—Z-80程序。

In this paper, based on the relation between the weighting matrices in linear quadratic optimal regulator and closed loop poles, a combined design method is presented for the optimal system with excellent dynamical characteristics and robustness. Applying this method in the design of control system of a certain flying vehicle,the performance is significantly improved.

本文根据线性最优调节器加权阵与闭环系统极点的关系,提出了一种综合最优系统设计法,使系统同时具有良好的动特性和较强的鲁棒性。文中应用这种方法对某型飞行器控制系统进行了设计,使飞行器性能指标得到了显著提高。

A technique using the principle of dynamic programming was developed for designing optimal flight test inputs for aircraft or missile Aerodynamic parameter estimation experiments. The optimal inputs were multi-step signal, which could be produced easily,and it reached optimality in the mean of accuracy. The technique had made it possible to include practical output constraint to avoid model invalid caused by large maneuver. An example was presented here for a linear model describing the lateral dynamics of an...

A technique using the principle of dynamic programming was developed for designing optimal flight test inputs for aircraft or missile Aerodynamic parameter estimation experiments. The optimal inputs were multi-step signal, which could be produced easily,and it reached optimality in the mean of accuracy. The technique had made it possible to include practical output constraint to avoid model invalid caused by large maneuver. An example was presented here for a linear model describing the lateral dynamics of an aircraft, showing the validity of the approach.

用动态规划法设计了旨在提高飞行器气动参数辨识精度的最优方波形输入信号。设计出的信号不仅在工程上易于实现,还在精度意义上达到了最优。为了避免加输入信号后飞行器状态离开线性工作点,从而导致模型失效,该设计方法还考虑了输出约束。用于某型飞行器的输入信号设计结果表明,该法是有效的。

 
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