论文部分内容阅读
飞航导弹模型可以处理成一种四层非线性、时变块对角结构， 但其中一、二层模型不是仿射型模型， 这在控制理论的应用上受到限制。应用优化线性化理论对这两层模型进行仿射型处理， 这样就得到了飞航导弹的四层非线性仿射型模型。这种模型非常适用于一些控制理论的应用， 例如， 可以采用变结构控制理论来实现对导弹的分层控制。
The flight-guided missile model can be processed into a four-layer nonlinear and time-varying block diagonal structure. However, the first and second layer models are not affine models, which limits the application of control theory. Applying the theory of optimized linearization to affine the two-layer model, the four-layer nonlinear affine model of the missile is obtained. This model is very suitable for the application of some control theory. For example, the variable structure control theory can be used to realize the layered control of missiles.