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     A systematic design method for flight trajectory command integrated tracker of tactical mission integrated flight management system(TMIFMS) is developed through the multiple time scale singular perturbation method combined with dynamic inverse decoupling control theory and optimal decoupling control law theory for optimal linearization system in a small neighborhood of a dynamic equilibrium point.
     运用多重尺度奇异摄动理论,结合动态逆解耦理论和动态平衡点邻区域优化线性化系统的优化解耦控制律理论,研究了战术任务综合飞行管理系统的综合飞行轨迹指令跟踪控制器系统化设计方法。
短句来源
     Using the global 2°×2.5° grid data, the local 30′×30′ grid data [1] obtained from weather stations in China area and its vicinity, and Farrell's loading theory of elastic earth model method, study the influences of surface gravity due to air pressure changes. The air pressure corrections of the Wuhan earth's tidal observation have been calculated by numerical integrating to compute the expressions.
     利用全球 2°× 2 .5°、中国及邻区域 30′× 30′气压资料和 Farrell弹性地球模型负荷理论 ,采用数值积分方法 ,计算了大气压力变化对武汉台站重力场观测的影响。
短句来源
     A systematic design method for integrated flight trajectory command tracker of Tactical Mission Integrated Flight Management System(TMIFMS) is developed through the multiple time scale singular perturbation method combined with dynamic inverse decoupling control theory and optimal decoupling control law theory for optimal linearization system in a small neighborhood of a dynamic equilibrium point. A controller for F 15 fighter is designed with the method. The results of digital simulation show that the controller can control fighter track commands in different time scale.
     运用多重尺度奇异摄动理论,结合动态逆解耦理论和动态平衡点邻区域优化线性化系统的优化解耦控制律理论,研究了战术任务综合飞行管理系统的综合飞行轨迹指令跟踪控制器系统化设计方法.对F-15飞机,设计了综合飞行轨迹跟踪控制器.数字仿真结果表明,设计的跟踪控制器能够控制飞机精确跟踪不同时标集的飞行指令.
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  相似匹配句对
     The Regional Dimension
     关于区域
短句来源
     FEATURES OF GRAVITY AND MAGNETIC FIELDAND REGIONAL TECTONICS OF YELLOW SEAAND ITS ADJACENT AREA
     黄海和区重磁场及区域构造特征
短句来源
     Outline of regional geological setting
     区域地质概况
短句来源
     SOME FEATURES OF THE RECENT TECTONIC STRESS FIELD OF CHINA AND ENVIRONS
     中国及区现代构造应力场的区域特征
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     SYNTHESIS OF o-CHLOROACETOPHENONE
     氯苯乙酮的合成
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  neighborhood region
Statistical analysis on energy field of seismicity in Ningxia and its neighborhood region
      
Taking the regional seismicity energy as the random function of space and time, the features of small seismicity field in Ningxia and its neighborhood region are studied by the analytical method of natural orthogonal function expansion.
      
Another type of independent variable is called an areal variable, which represents the area of a neighborhood region of points.
      
Each sensor works as a sensing collaborator, which senses its neighborhood region for the targeted activity.
      
Finally, a feature descriptor is computed from each neighborhood region.
      
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A systematic design method for integrated flight trajectory command tracker of Tactical Mission Integrated Flight Management System(TMIFMS) is developed through the multiple time scale singular perturbation method combined with dynamic inverse decoupling control theory and optimal decoupling control law theory for optimal linearization system in a small neighborhood of a dynamic equilibrium point. A controller for F 15 fighter is designed with the method.The results...

A systematic design method for integrated flight trajectory command tracker of Tactical Mission Integrated Flight Management System(TMIFMS) is developed through the multiple time scale singular perturbation method combined with dynamic inverse decoupling control theory and optimal decoupling control law theory for optimal linearization system in a small neighborhood of a dynamic equilibrium point. A controller for F 15 fighter is designed with the method.The results of digital simulation show that the controller can control fighter track commands in different time scale.

运用多重尺度奇异摄动理论,结合动态逆解耦理论和动态平衡点邻区域优化线性化系统的优化解耦控制律理论,研究了战术任务综合飞行管理系统的综合飞行轨迹指令跟踪控制器系统化设计方法.对F-15飞机,设计了综合飞行轨迹跟踪控制器.数字仿真结果表明,设计的跟踪控制器能够控制飞机精确跟踪不同时标集的飞行指令.

A systematic design method for flight trajectory command integrated tracker of tactical mission integrated flight management system(TMIFMS) is developed through the multiple time scale singular perturbation method combined with dynamic inverse decoupling control theory and optimal decoupling control law theory for optimal linearization system in a small neighborhood of a dynamic equilibrium point. A controller for F 15 fighter is designed with the method. The results...

A systematic design method for flight trajectory command integrated tracker of tactical mission integrated flight management system(TMIFMS) is developed through the multiple time scale singular perturbation method combined with dynamic inverse decoupling control theory and optimal decoupling control law theory for optimal linearization system in a small neighborhood of a dynamic equilibrium point. A controller for F 15 fighter is designed with the method. The results of digital simulation show that the controller can control fighter track commands in different time scales.

运用多重尺度奇异摄动理论,结合动态逆解耦理论和动态平衡点邻区域优化线性化系统的优化解耦控制律理论,研究了战术任务综合飞行管理系统的综合飞行轨迹指令跟踪控制器系统化设计方法。对F-15飞机,设计了综合飞行轨迹跟踪控制器。数字仿真结果表明,设计的跟踪控制器能够控制飞机精确跟踪不同时标集的飞行指令。

Using the global 2°×2.5° grid data, the local 30′×30′ grid data [1] obtained from weather stations in China area and its vicinity, and Farrell's loading theory of elastic earth model method, study the influences of surface gravity due to air pressure changes. The air pressure corrections of the Wuhan earth's tidal observation have been calculated by numerical integrating to compute the expressions. The result shows that the volume is up to 12 μGal(1 Gal=1 cm/s 2). That is means we need air pressure corrections...

Using the global 2°×2.5° grid data, the local 30′×30′ grid data [1] obtained from weather stations in China area and its vicinity, and Farrell's loading theory of elastic earth model method, study the influences of surface gravity due to air pressure changes. The air pressure corrections of the Wuhan earth's tidal observation have been calculated by numerical integrating to compute the expressions. The result shows that the volume is up to 12 μGal(1 Gal=1 cm/s 2). That is means we need air pressure corrections to improve high precision observations such as superconducting gravimeter or FG5 absolute gravity meter. In comparison of the atmospheric gravity admittance obtained from tides analyses with our result, we find they are very close. Therefore, air pressure correction can be calculated by air pressure at the station and the atmospheric admittance from our model results.

利用全球 2°× 2 .5°、中国及邻区域 30′× 30′气压资料和 Farrell弹性地球模型负荷理论 ,采用数值积分方法 ,计算了大气压力变化对武汉台站重力场观测的影响。对 1990年 1月 1日至 12月 31日的数值结果分析表明 ,全球大气压力变化对武汉台站重力的影响峰对峰达 12微伽 ,大气重力导纳的年平均值为 -0 .2 6 0μGal/mba(1mba=1h Pa) ,这一结果同潮汐分析中由回归分析方法获得的导纳值相近。说明在利用超导重力仪观测资料应用于地球动力学研究之前 ,有必要作精细的全球气压变化改正

 
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