前言以比例导航作为导引方法的现有国外空—空导弹,都是以攻击小机动空中目标为其特征的。越南、中东战场上的战例说明,未来空—空导弹的主要问题是有效地攻击大机动目标。为此,增大导弹机动能力,例如,双鸭与双三角气动力面的改进,就是对付那些以产生大的横向加速度为特点的空中目标的,推力矢量控制与推力矢量与振幅控制技术的研 Foreword Existing foreign air-to-air missiles that use proportional navigation as a guidance method are characterized by attacks on small-maneuvered air targets. Vietnam, the battle scenario on the Middle East shows that the main problem of future air-to-air missiles is to effectively attack large maneuver targets. To this end, to increase missile maneuverability, for example, double-duck and double-delta aerodynamic surface improvements, is to deal with those to produce large lateral acceleration characteristics of the air target, thrust vector control and thrust vector and amplitude control technology research