Chinese translation for "扰动力矩"
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- disturbance torque
disturbing moment
Related Translations:
扰动量: disturbance quantitydisturbed quantitydisturbing quantity 扰动稳定性: stability for disturbance 结构扰动: structural disturbancesstructural perturbation 低头扰动: nose-down disturbance 轴对称扰动: axisymmetric disturbance 边界扰动: boundary distrubance
- Example Sentences:
| 1. | 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。 | | 2. | 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。 | | 3. | 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。 | | 4. | 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。 | | 5. | 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。 |
- Similar Words:
- "扰动矩阵" Chinese translation, "扰动空气" Chinese translation, "扰动控制系统" Chinese translation, "扰动理论" Chinese translation, "扰动力" Chinese translation, "扰动量" Chinese translation, "扰动零输出" Chinese translation, "扰动流" Chinese translation, "扰动流函数" Chinese translation, "扰动流体能量" Chinese translation
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