CAJ | 학술논문

针对飞机实际飞行中的各种随机抖动，提出了一种飞机动态RCS序列仿真方法。首先采用飞机缩比模型的激光测量尺寸在FEKO中建立精确电磁计算模型，得到了飞机全空域静态RCS数据。在运动建模中先设定飞行航迹，推算出飞行过程中飞机的姿态角变化，叠加实际飞行中随机抖动的影响，使得运动建模更加贴近实际。仿真结果表明：叠加随机抖动后的动态RCS与初始值相差3 dB的点数占总数的17．5％，该方法对雷达目标动态特性的仿真研究具有重要的参考价值。
침대비궤실제비행중적각충수궤두동，제출료일충비궤동태RCS서렬방진방법。수선채용비궤축비모형적격광측량척촌재FEKO중건립정학전자계산모형，득도료비궤전공역정태RCS수거。재운동건모중선설정비행항적，추산출비행과정중비궤적자태각변화，첩가실제비행중수궤두동적영향，사득운동건모경가첩근실제。방진결과표명：첩가수궤두동후적동태RCS여초시치상차3 dB적점수점총수적17．5％，해방법대뢰체목표동태특성적방진연구구유중요적삼고개치。
Considering the random jitter of a flying aircraft,a simulation method for dynamic RCS series of aircraft was proposed .An electromagnetic calculation model of the aircraft based on scaling model size was established in FEKO,and the all-space static RCS was obtained .After the flight path was simulated and the attitude angle of the aircraft in flight was calculated out,the dynamic RCS series of the aircraft flying with random jitter were obtained .Random jitter was considered in movement modeling to make movement more realistic.The simulation results show that there are 17.5% points that have 3 dB or above difference with the initial RCS value after considering the effect of the random jitter .The presented method is beneficial to the study of dynamic characteristics of radar targets .