摘要
首先将外层空间导弹姿态控制系统非线性模型的六个状态变量分别进行线性变换及非线性变换, 然后采用非线性状态反馈方法将原非线性系统变换为一渐近稳定的线性系统, 得到了相应的非线性姿态控制律。
First, the 6-rank nonlinear model's state variables of the outerspace missile attitudes control system are transformed by employing linear and nonlinear transformation. Then, with the nonlinear state feedback method, an asymptotically stablized linear system is obtained corresponding the former nonlinear one. Meanwhile, the nonlinear attitudes control law is also derived. Finally, the simulation result proves the validity of this control method.
出处
《航天控制》
CSCD
北大核心
1999年第4期6-10,共5页
Aerospace Control
