Control System Of Missile Design And Simulation

With the rapid development of electrical technology and computer technology, the SINS (the strap- down inertial navigation system )/GPS (the global position system)combined guidance has developed fast. Because it has many advantages, it represents the future developing direction of the missile's guidance. Nowadays, there isn' t the missile, which uses the SINS / GPS combined guidance in our country. Thus, it is necessary to study the control system, which adopts the SINS / GPS combined guidance.Form the practical demand, this paper studies the guided method and the control system for the missile which uses the SINS / GPS combined guidance. The study in this thesis has practical value and utility value.The theory of the composite guidance is described firstly. And the SINS / GPS combined guidance are discussed in detail. Secondly, the paper explicate the specialty of the rotary missile. In this paper, the following works have been done:l.Form the rotary missile concept, the mathematic model of the missile has been established.2.The Control System has designed in this paper. And it includes two way: the schema trajectory and the proportion guidance. 3. The Control System has designed in this paper. 4.At last, aiming to a practical application in engineering桾he missile, the trajectory is simulated.