为达到高机动性,过去长时间研究的正常式导弹的弹翼必须相当大。本文利用鸭式空空导弹(XAAM-3)的研究成果,探讨了小型高机动性鸭式导弹的气动外形。结果证明,使用较小的弹翼同样可以达到高机动性的目的。为此,必须在俯仰面上仅操纵升降舵,在偏航而上仅操纵方向舵和副骥,导弹必须具有90°转弯控制(BTT)能力。实验证明,这种导弹的各种性能比过去探讨的正常式导弹的性能更好。 To achieve high maneuverability, normal missile missiles that have been studied for a long time must be quite large. In this paper, the aerodynamic shape of a small-sized, high-mobility Duck missile is discussed using the research results of the Duck-type air-to-air missiles (XAAM-3) The results show that the use of smaller wing also can achieve the purpose of high mobility. To do so, only the elevator must be maneuvered on the pitch plane and only the rudder and vice versa must be yawed, and the missile must have a 90 ° turn control (BTT) capability. Experiments show that the performance of such missiles is better than that of normal missiles explored in the past.