According to the direction and damping characteristic of the torque produced by the magnetic torques the three-axis attitude control schemes of gravity gradient satellite and other satellite with damper were put forward in this paper .

根据磁 力矩在地磁场中的定向阻尼特性，提出了磁控重力 梯度和有阻尼器的非重力 梯度卫星姿态控制律。

Through the simulation the influence of the aero torque and the gravity gradient torque in the process of the relocation is analyzed the request of the relocation process to the space station control is analyzed .

仿真分析了转位过程中气动 力矩和重力 梯度力矩的影响，分析了转位过程对空间站姿态控制执行机构提出的要求。

Microsatellite Passivity Attitude Control Using Aerodynamic Torque and Gravity Gradient

气动 力矩和重力 梯度 矩实现微小卫星三轴姿态控制

Positive torque is only produced at angles when the inductance gradient is positive .

正面 扭矩只导致在角度当感应性 梯度是正面的。

Secondly the dynamic features surplus torque and loading gradient features of PTSS are analyzed by the couple model between the rudder and the EALS .

然后，采取把系统模型转化为舵机和负载模拟器相互耦合作用的形式，对被动式力矩伺服系统动态特性、多余 力矩和加载 梯度一一进行理论分析，得出：多余力矩与舵机运动 速度直接相关；