本发明涉及一具有推力矢量和气动控制的喷气推进导弹,这两个控制通过同样的装置进行调节,而且更特别的是,本发明是指控制部局的。既有推力矢量控制又有气动控制的导弹的优点不同于只用推力矢量控制的导弹那样,这种导弹可在喷气发动机完成主动段以后及在弹道开始的时候进行控制。也不同于只用气动力控制的导弹那样,这种导弹前后 The present invention relates to a propellant projectile having thrust vectoring and pneumatic control, both controlled by the same means, and more particularly to the control unit. The advantages of both thrust vector control and aerodynamically controlled missiles are different from those of thrust-vector-only missiles that can be controlled after the jet engine completes the active segment and at the beginning of the trajectory. It is also different from the aerodynamic-only missiles, which are the front and rear missiles