CAJ | 학술논문

针对起飞质量对小型导弹总体参数设计的制约问题，以最小起飞质量为目标函数，应用复合形法，对小型飞航导弹纵向平面运动的方案弹道进行了总体参数优化设计研究。研究中考虑了法向过载、射程、最大速度、末速度、巡航高度和导弹离轨速度等因素。仿真结果表明：优化之后，导弹在飞行过程中的各特性参数满足总体指标要求的同时，实现了导弹起飞质量最小的目标。
침대기비질량대소형도탄총체삼수설계적제약문제，이최소기비질량위목표함수，응용복합형법，대소형비항도탄종향평면운동적방안탄도진행료총체삼수우화설계연구。연구중고필료법향과재、사정、최대속도、말속도、순항고도화도탄리궤속도등인소。방진결과표명：우화지후，도탄재비행과정중적각특성삼수만족총체지표요구적동시，실현료도탄기비질량최소적목표。
In order to solve the restriction of the take-off mass to the overall parameter design of the small winged missile, this paper takes the minimum take-off mass as the object function , employs complex optimization to opti-mize the overall parameters of the small winged missile's project trajectory in the vertical planar movement .The fol-lowing factors have been researched:the normal overload, range, the maximum and the terminal velocity , and the cruising altitude and off-track velocity .Simulation results show that the characteristic parameters during the flight can meet the overall indicators and achieve the minimum take-off mass after the optimization .