扰动力矩的英文

• disturbance torque
• disturbing moment

• "扰动"英文翻译    excitation; turbulent motion ...
• "力矩"英文翻译    force moment; moment; moment ...
• "波浪扰动力矩" 英文翻译 :    wave exciting moment
• "滚动扰动力矩" 英文翻译 :    disturbance rolling moment
• "横摇扰动力矩" 英文翻译 :    roll-excitation moment
• "扰动力" 英文翻译 :    destabilizing force; disturbing force; force，disturbing
• "动力矩" 英文翻译 :    dynamic torque
• "波浪扰动力" 英文翻译 :    wave exciting force
• "动力扰动" 英文翻译 :    energetic disturbance
• "附加扰动力" 英文翻译 :    additional distrubing force; additonal disturbing force
• "广义扰动力" 英文翻译 :    generalized excitation
• "气动力扰动" 英文翻译 :    ad aerodynamic disturbance
• "变动力矩" 英文翻译 :    fluctuating moment
• "传动力矩" 英文翻译 :    drive moment; drive torque; driver torque; driving moment
• "电动力矩" 英文翻译 :    electrokinetic moment
• "动力矩阵" 英文翻译 :    dynamic matrix
• "滚动力矩" 英文翻译 :    roll moment; rolling moment
• "滑动力矩" 英文翻译 :    slimoment
• "激动力矩" 英文翻译 :    exciting moment
• "进动力矩" 英文翻译 :    moment of precession; precession
• "空气动力矩" 英文翻译 :    aerodynamic couple; aerodynamic moment
• "扭动力矩" 英文翻译 :    torque
• "起动力矩" 英文翻译 :    anzugsmoment fixturing torque / clamping torque/tightening torque; starting torque coefficient
• "启动力矩" 英文翻译 :    starting moment; starting torque
• "气动力矩" 英文翻译 :    aerodynamic moment; aerodynamical moment

• The dynamic lag error of servo system , the error caused by disturbing moment and the influence of ship motion to tracking performance are also described
  同时，给出伺服系统动态滞后误差、扰动力矩产生的跟踪误差，以及由于舰船运动对跟踪性能的影响。
• Through an application of the improved nonlinear vks model based on complex modulus , for the cases of general connections and inter - blade connections for the nonlinear elastomeric lag dampers , the small disturbance momental equation is given
  采用基于复模量的非线性vks改进模型，建立叶间粘弹减摆器和普通连接粘弹减摆器的小扰动力矩方程。
• Secondly , for satellite controlled by reaction wheels , an algorithm or strategy is presented . and then reaction wheels are used to generate a known disturbance torque , using thrusters as controller and gyro as the attitude sensor , a thruster parameters calibration for thruster levels and alignments on - line is achieved
  其次,针对反作用飞轮控制的卫星,提出了一种卫星质量特性在线辨识策略和辨识算法,并利用反作用飞轮产生扰动力矩,推力器作为控制执行机构,使用陀螺测量卫星姿态角速度,实现推力器推力大小和方向等参数的在线辨识。
• So . the low speed jitter problem has been the central task in the servo system research . the improvement of the working precision at low speed is hindered by the disturbances of the friction moment and the motor torque wave , while the decrease of the disturbances is restricted by the making technology . for the reason , the research of the low speed properties and corresponding compensation methods means a lot for the optoelectronic tracking system
  转台伺服系统低速工作精度主要受到以摩擦力矩、电机波动力矩为主的扰动力矩的影响，而摩擦力矩、电机波动力矩的减小又受到转台制造工艺水平的限制，所以，转台伺服系统的低速特性以及抖动补偿研究，对结构简单、性能优良的精密光电跟踪系统的研制，具有相当重要的意义。
• Lastly , establish the rigid - body spaceship attitude kinematics and dynamics equations , and primarily design the spaceship attitude law including limit loop parameters and two kind switch curves . analyze the astronaut ’ s disturbance moments . put the disturbance moments of typical astronaut ’ s push - off act as the input datas of the control system simulation , and analyze the response of the attitude control system after disturbed
  最后,建立刚体飞船姿态运动学及动力学方程,并对飞船姿态控制律进行了初步的设计,包括极限环参数的设计和两类典型的开关曲线的设计;对航天员扰动力矩进行了分析;以典型的航天员推离动作对飞船的扰动力矩作为控制系统仿真的输入参数,分析姿态控制系统受到扰动后的响应。