Computer Controllment of Von Neumann Model on Civil Aviation Industry

The problem of computer control algorithm for the singular Von Neumann input-output model on civil aviation industry is researched. A kind of new mathematic method is applied to study the singular systems without converting them into general systems. A kind of stability condition under which the singular input-output model is admissible is proved with the form of linear matrix inequality. Based on this, a new state feedback stability criterion is established. Then the formula of a desired state feedback controller is derived.