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flight envelope
飞行包线:描述飞行器在特定飞行状态下的性能极限的图形表示
常用释义
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基本释义
  • 飞行包线:描述飞行器在特定飞行状态下的性能极限的图形表示,包括速度、高度、马赫数等参数。
例句
  • 1·Results Aero engine linear model within flight envelope designed point and active fault-tolerant controller.
    结果得到在飞行包线设计点发动机线性模型和主动容错控制器。
  • 2·It is also an active throttle, which means it provides feedback to the pilot as a function of flight envelope and flight mode.
    它同时还是一个主动的油门,这是指它可以根据飞行包线和飞行模式的函数为飞行员提供反馈。
  • 3·The belly-mounted system is remotely operated and capable of delivering accurate, sustained fire throughout the CV-22's flight envelope.
    该系统位于机腹,通过远端操作工作,能够在CV-22飞机的整个飞行过程中提供精确的、持续的火力保护。
  • 4·As a hypersonic propulsion system, turbo-ramjet received recognition because of the widely flight envelope and excellent performance such as Isp.
    在高超声速推进系统中,涡轮冲压组合发动机由于有着宽广的飞行范围,良好的比冲性能,受到世界各国的普遍重视。
  • 5·The active stick and throttle allows realtime control shaping to optimize feel and aircraft response as a function of current flight envelope and mode.
    主动驾驶杆和油门杆允许针对当前飞行包线和模式实时地进行控制调整以优化操作感受和飞机响应。
  • 6·The team is focused on researching the low-speed characteristics of the design and expanding its flight envelope beyond the limits of current capabilities.
    该小组是侧重于研究低速的特点,设计并扩大其飞行包线范围外的能力。
  • 7·Furthermore, without changing the structure and parameters of controller in big flight envelope, our scheme can simplify the design of flight control system.
    直接针对飞机的非线性模型设计的自抗扰控制器在很大的包线范围内不需要改变控制器的结构和参数,简化了设计过程。
  • 8·Furthermore, the design of flight control system is simplified by the scheme proposed without changing the structure and parameters of controller in big flight envelope.
    直接针对飞机的非线性模型设计的自抗扰控制器在很大的包线范围内不需要改变控制器的结构和参数,简化了设计过程。
  • 9·Qualification issues include design and testing required to maintain the combat capabilities of the UH-60 Black Hawk and the safe flight envelope of the aircraft with the tank.
    该机的设计难点在于用户要求既要保持UH-60原有的攻击运输能力,又要在携带外部大型水箱的情况下保持飞行安全。
  • 10·Using neutral networks, the relationship between engine flight conditions, states and the parameters of controller are fitted, and the controller characteristics in full flight envelope are verified.
    利用神经网络拟合发动机飞行条件、状态与控制器参数之间的关系,验证了控制器在全飞行包线内的性能。