气动力矩的英文

• aerodynamic moment
• aerodynamical moment

• "矩"英文翻译    carpenter's square; square r ...
• "空气动力矩" 英文翻译 :    aerodynamic couple; aerodynamic moment
• "滚转气动力矩" 英文翻译 :    aerodynamic rolling mmoment couple
• "空气动力力矩" 英文翻译 :    aerodynamic moment; air moment
• "纯空气动力力矩" 英文翻译 :    pure aerodynamic couple
• "空气动力恢复力矩" 英文翻译 :    aerodynamic restoring moment
• "空气动力矩分量" 英文翻译 :    component of aerodynamic moment
• "空气动力矩基准点" 英文翻译 :    moment reference
• "空气动力力矩分量" 英文翻译 :    component of aerodynamic moment
• "气动力矩平数据" 英文翻译 :    rotary-balance aerodynamic data
• "空气动力矩阵计算程序" 英文翻译 :    aerodynamic matrix procdeure
• "动力矩" 英文翻译 :    dynamic torque
• "气动力" 英文翻译 :    aerodynamic force; airfoil; airforce
• "气动力，空气动力" 英文翻译 :    aerodynamic force
• "按非线性化理论求空气动力矩" 英文翻译 :    nonlinear aerodynamic moment formulation
• "地面效应对气动力矩的影响" 英文翻译 :    ground effect on the moment
• "对平均空气动力弦处的俯仰力矩" 英文翻译 :    pitching moment about
• "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

• First , a great deal of aerodynamics and moment parameters are processed by look - up table , and then the flight simulation model of normal aircraft and fault aircraft are established
  首先,利用look - uptable对大量的气动力参数及气动力矩参数数据进行了插值处理,并在此基础上建立了正常和故障飞机飞行的仿真模型。
• The structural vibrational equations for the former are also depicted . the disturbance torques imparted by space environment are analyzed , which include gravity gradient torque , solar pressure torque , aerodynamic torque and magnetic torque
  对作用在卫星上的各种空间环境力矩进行了分析,包括重力梯度力矩、太阳光压力矩、气动力矩、剩磁力矩等。
• Through the analysis of attitude dynamic equation , how to realize three axis passivity stabilization of the mircrosatellite by just using environmental torque is presented . three sorts conformations of three axis passivity stabilization of the mircrosatellite by using environmental torque are put forward , one is to realize the passive attitude control of microsatellite by using the aerodynamic moment and the gravity gradient , the other two by making use of the gravity gradient and the geomagnetic moment , the attitude dynamics of microsatellite of the three sorts are analysed in detail
  通过对卫星姿态动力学方程分析，给出如何利用环境力矩实现微小卫星三轴姿态被动稳定，并提出三种利用环境力矩实现微小卫星三轴姿态被动稳定方案，即一种利用气动力矩和重力梯度实现微小卫星三轴姿态被动稳定方案和两种利用重力梯度和地磁力矩实现微小卫星三轴姿态被动稳定方案，对采用这三种方案的卫星的姿态运动进行详细分国防科技大学研究生院学位论文析。