The proposed method is applied to satellite attitude controller design to cope with the errors arising while linearizationprocedure.
将所得结果应用于卫星姿态控制系统的设计，以解决对模型进行线性化处理时产生的误差。
2
From the linearizationprocedure, a new approach of system identification that is on-line real time modeling and real time feedback control correction can be found.
In this sense for a nonlinear process the on-line identification is necessary and corresponding to a quasi-linearization or a sequential linearizationprocedure of process.