CAJ | 학술논문

根据中远程导弹制导系统大都采用脉冲多卜勒雷达导引头的趋势和中远程防空导弹末制导实现对目标机动运动状态的需求，基于目标螺旋机动和蛇行机动的切向加速度和法向加速度在目标轨迹活动框架上缓变的特点，本文提出了一种建立在目标轨迹活动框架上的运动状态方程和自适应Kalman估计算法，该方法克服了在直角坐标系和球坐标系上估计目标快变加速度机动延迟大的缺陷。仿真实验证明该算法有很好的跟踪稳定性和收敛性，为先进末制导律的实现创造了条件。
근거중원정도탄제도계통대도채용맥충다복륵뢰체도인두적추세화중원정방공도탄말제도실현대목표궤동운동상태적수구，기우목표라선궤동화사행궤동적절향가속도화법향가속도재목표궤적활동광가상완변적특점，본문제출료일충건립재목표궤적활동광가상적운동상태방정화자괄응Kalman고계산법，해방법극복료재직각좌표계화구좌표계상고계목표쾌변가속도궤동연지대적결함。방진실험증명해산법유흔호적근종은정성화수렴성，위선진말제도률적실현창조료조건。
To meet the demand of terminal guidance of the medium-long range antiaircraft missile for target state, a new target state model and an adaptive Kalman estimating algorithm for radar homing missile attacking maneuvering target is proposed, with seeker radar adopted pulse doppler radar guidance system, based on the slowly changing of the tangential acceleration and the normal acceleration of the spiral maneuvering and snaking maneuvering in target trace frame coordinate system. It resolves the backward of long delay in fast-changed acceleration of target tracking in Cartesian coordinates or spherical coordinates. Simulation of one missile control and guide system proved its good stability and convergence, which will be very valuable for engineering accomplishing the advanced terminal guidance law.