controlled response中文是什么意思

• 有节制的反应
• 有控制的反应

• "control"中文翻译    n. 1.支配，管理，管制，统制，控制；监督。 2.抑制 ...
• "response"中文翻译    n. 1.回答，答复。 2.【宗教】应唱圣歌。 3. ( ...
• "response curve of controlled plant" 中文翻译 :    调节对象飞升曲线; 调节对象正升曲线
• "controlled" 中文翻译 :    被调节的; 管制的，被控制的; 可控的; 克制的; 受控的; 受控访问性; 受控制的；受管制的；受节制的; 受约束的; 自制的
• "be response for" 中文翻译 :    对负责; 对……负责，是造成……原因; 是…造成; 是造成……原因
• "in response to" 中文翻译 :    对回应; 回答反应; 响应，反应; 响应，回答; 作为对…的反应
• "no response" 中文翻译 :    不响应; 没有响应
• "no-response" 中文翻译 :    无响应, 无应答
• "on-response" 中文翻译 :    “给”反应,给反应
• "response" 中文翻译 :    n. 1.回答，答复。 2.【宗教】应唱圣歌。 3. (因刺激等引起的)感应，反应，反响；应验；【物理学】响应；【无线电】灵敏度，感扰性；特性曲线。 His oratorical efforts evoked no response in his audience. 他的雄辩在听众中不起反响。 call forth no response in sb.'s breast 在某人心中不起反应。 in response to 应…而，答…而。 make no response 不回答。
• "response to" 中文翻译 :    对…的回答; 对……的回答,反应; 对…的反应
• "aerodynamically controlled" 中文翻译 :    空气动力操纵的
• "aerodynamically-controlled" 中文翻译 :    空气动力操纵的
• "air controlled" 中文翻译 :    空气控制的; 气动的; 气控
• "air-controlled" 中文翻译 :    空气操纵的; 空气控制的; 气动操纵的; 气动的
• "aircraft controlled" 中文翻译 :    机上控制的
• "aircraft-controlled" 中文翻译 :    机上控制的
• "airflow controlled" 中文翻译 :    空气流量控制
• "bacterially controlled" 中文翻译 :    细菌控制的
• "be controlled by others" 中文翻译 :    受人支配
• "central controlled" 中文翻译 :    集中控制的
• "computer controlled" 中文翻译 :    电脑控制; 计算机控制的
• "controlled 4wd" 中文翻译 :    可变扭力分配式电子控制四轮驱动
• "controlled a ociation" 中文翻译 :    控制联想
• "controlled access" 中文翻译 :    受控访问

• The first is called output caching , which allows you to store dynamic page and user control responses
  第一种称为输出缓存，它允许您存储动态页和用户控制响应。
• One - cycle control response fast , it can reject power perturbations and the control circuit is simple and reliable
  单周控制法具有响应快、抗电源干扰和控制电路简单可靠等优点。
• The simulation experiment indicated that the method can solve the time lag of the control response in
  仿真实验表明,该智能复合控制方法能够很好的解决红外干燥箱温度控制响应滞后的问题。
• It includes reducing the density of medicines , choosing the optimal medicine proportion , choosing unpolluted catalyst and controlling response time properly
  其中包括降低药品浓度；选择最佳药品是配比；选择无污染的催化剂；合理控制反应时间。
• A hysteresis - band instantaneous current control pwm technique is popularly used because of its simplicity of implementation , fast current control response , and inherent peak current 1 imiting capability
  瞬时电流滞环控制技术由于实现简单、响应速度快和具有自然限流等优点而得到广泛应用。
• The first is output caching , which allows you to store dynamic page and user control responses on any http 1 . 1 cache - capable device in the output stream , from the originating server to the requesting browser
  第一种类型是输出缓存，它允许将动态页和用户控件响应存储在输出流（从发起服务器到请求浏览器）中任何具备http 1 . 1缓存功能的设备上。
• The superposition between the helicopter rotor induced flow and the warship airwake leads to the formation of the complex wake , which affects the helicopter ' s control response and flight safety during take - off and landing from a warship
  摘要直升机旋翼诱导流与舰船空气尾流叠加后形成复合流场，对直升机舰上起降时的操纵响应及飞行安全有很大的影响。
• Nomura giko s genesis superheated steam generation device is equipped with a superb temperature control response capability thanks to the use of an originally developed heating element structure , and is also able to generate larger volumes of superheated steam than similar devices by other makers
  野村技工的过热蒸汽发生装置, genesis运用我们独自开发的发热体构造，可实现高速温度控制应答，与以往公司不同的是该装置可生成大容量的过热蒸汽。
• The approach maintains the simplicity of the original algorithm , and carry out perfect model following . the pseudo - inverse method is concerned with distributing the deflection commands of multiple control surfaces of the aircraft to generate required control responses when the number of independent control surfaces is greater than the number of required independent control responses
  伪逆算法通过改变反馈增益来实现故障系统的控制律重构，当一个操纵面发生故障后，可改变控制律重新分配控制指令，利用其它操纵面来实现它的功能，近代先进飞机多采用此方法来提高飞机的容错能力。
• This model is formulated as a non - linear state - space representation of helicopter flight dynamics , incorporating with blade element unsteady aerodynamics , a finite state dynamic inflow wake model , and flapping / lead - lag blade dynamic model . the formulation of the coupled rotor and fuselage equations enables the use of common solution techniques for trim and linearization in arbitrary steady flight condition as well as control response calculations
  本项研究针对新机研制过程必须解决的品质评定、飞控系统设计等问题，按照ads - 33军用品质规范的要求，建立了一个较完整的直升机非线性的、具有状态空间表达形式的飞行动力学模型，进行了模型验证工作，并以某样例直升机为例，计算了ads - 33品质规范（ 3

• controlled response meaning