As inertial actuators mounted on the spacecraft, Single Gimbal control Moment Gyroscopes (SGCMGs) can affect the attitude control accuracy to a great extent.
作为应用在航天器上的惯性执行机构，单框架控制力矩陀螺(SGCMG)的操纵性能对航天器姿态控制精度有着极大的影响。
The simulation result shows that the variable structure automatic pilot for KKV is fast and has high attitude control accuracy, which satisfies the requirements.
数学仿真表明，变结构自动驾驶仪具有很好的快速性和很高的姿态控制精度，可以满足动能拦截器对姿态控制的要求。
Then, base on the problem of attitude control of a satellite under development, we design a NN compensation controller for high accuracy orientation phase.
然后，基于某型小卫星的姿态控制问题，设计了高精度定向阶段的神经网络补偿控制器。
应用推荐