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post stall maneuver
相关语句
  过失速机动
     A Study on the Thrust Vectoring Control and Aircraft's Post Stall Maneuver
     推力矢量控制与飞机过失速机动仿真研究
短句来源
     This paper discussed the application of this method in the design of flight control system for the post stall maneuver.
     针对过失速机动飞机探讨了非线性动态逆方法在飞行控制系统设计中的应用。
短句来源
     Simulation result shows that the control law is effective for the post stall maneuver design of modern aircrafts.
     仿真实验表明 ,这种控制律用于现代飞机的过失速机动是有效的 .
短句来源
     This paper investigates the large angle attitude post stall maneuver control for the agile turn phase of an air-to-air missile that has high off-boresight capability and head reverse maneuverability.
     为研究具有大离轴角及越肩发射能力的先进空空导弹初始段敏捷转弯方法,研究了装有反作用喷气控制系统的空空导弹的大角度姿态过失速机动控制律。
短句来源
  “post stall maneuver”译为未确定词的双语例句
     Thrust vectoring control(TVC)is an important role for future aircraft toimprove agility and to acquire post stall maneuver(PSM).
     叙述了推力矢量控制的分类、发展过程,说明了推力矢量控制的重要性,推力矢量控制是未来战斗机提高敏捷性和获得过失速机动的重要手段。
短句来源
     A post stall maneuver control law for aircraft with new control surfaces and trust vectoring control is proposed.
     提出了一种多操纵面新气动布局飞机的过失速控制律设计方法 .
短句来源
     The control laws of the inner closed loop system and post stall maneuver are obtained through using symbol operations design.
     使用符号运算方法设计了系统闭环控制律和大攻角下的过失速控制律 .
短句来源
  相似匹配句对
     AGILITY AND POST-STALL MANEUVER
     敏捷性和过失速机动
短句来源
     Status and Trends of the Post Stall Maneuvers
     过失速机动的现状和发展趋势
短句来源
     Research on Optimal Post-stall Maneuvers
     过失速机动的优化
短句来源
     RESEARCH ON OPTIMAL POST STALL MANEUVERS
     最佳过失速机动研究
短句来源
     CONTROL REQUIREMENTS FOR POST STALL MANEUVERING
     过失速机动的操纵要求
短句来源
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The problems of agility and post stall maneuver, which have received extensive attention in recent years, are briefly depicted in this paper, including the presentation of these problems, the definition and metrics of agility, the main forms of unconventional (vectored) maneuver, the relationships between agility, combat effectiveness and flying qualities, the relationship between agility and aircraft design, etc.

对目前深受重视的敏捷性和过失速机动问题作了扼要介绍。内容包括:问题的提出:敏捷性的定义及其量度;非常规机动的形式;敏捷性与空战效率和飞行品质的关联:以及敏捷性与飞机设计的关联等。

Thrust vectoring control(TVC)is an important role for future aircraft toimprove agility and to acquire post stall maneuver(PSM).In this paper, the necessarity,definition and classified situation of TVC have been summarized.Moteovet,the benefitsacquired by vectored aircraft and several pr oblems faced with vectored aircraft have beenintroduced.

叙述了推力矢量控制的分类、发展过程,说明了推力矢量控制的重要性,推力矢量控制是未来战斗机提高敏捷性和获得过失速机动的重要手段。介绍了目前世界上航空发达的国家推力矢量控制和推力矢量喷管的发展现状和趋势,采用推力矢量控制和推力矢量喷管后使飞机所获得的效益和面临的问题。

In this paper the decoupling control theory for nonlinear multivariablesystems based on Differential Geometry Control Theory is introduced.A synthesis procedureof the decoupling control law for the nonlinear system is given. The calculation of equilibriumpoints for the nonlinear decoupled system is discussed.The stability of the decoupled closed-loop nonlinear system is also studied.Three forms of decoupling controls for aircraft nonlinear motion are studied with thedecoupling control theory.For the engineering...

In this paper the decoupling control theory for nonlinear multivariablesystems based on Differential Geometry Control Theory is introduced.A synthesis procedureof the decoupling control law for the nonlinear system is given. The calculation of equilibriumpoints for the nonlinear decoupled system is discussed.The stability of the decoupled closed-loop nonlinear system is also studied.Three forms of decoupling controls for aircraft nonlinear motion are studied with thedecoupling control theory.For the engineering application linear approximation of the aircraftnonlinear decoupling control law is discussed.Finally,three forms of agility maneuvers arerealized by three nonlinear decoupling control forms of aircraft motion and the results aresatisfying.The study will provide a new theoretical approach to investigate aircraft agility,the direct force control and post-stall maneuver of modern combat aircraft.

首先介绍了以微分几何控制理论为基础的非线性系统解耦理论,给出了解耦控制律的综合方法及解耦闭环系统平衡点的计算方法,井对解耦系统的稳定性进行了讨论。随后用非线性解耦理论研究了飞机非线性运动的三种解耦运动模式,并讨论了飞机非线性解耦控制律的线性近似解。最后用飞机非线性运动的三种解耦运动模式实现了三种形式的敏捷性机动,结果是满意的。为飞机敏捷性、直接力控制和过失速机动问题提供了一种理论研究方法。

 
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