CAJ | 학술논문

由于反辐射无人机的巡航特性，其高机动性对雷达诱偏系统设计提出了更高要求。在分析诱偏系统特点基础上，明确了系统设计要求，选用非相参的工作体制，并对系统组成进行了划分和功能描述。重点论述了诱偏系统的技术实现途径，通过对空域覆盖体制的分析，提出选用主瓣模拟副瓣的天线形式，描述了非相参体制雷达诱饵系统的工作流程，并对诱偏系统性能检验的试验方法和步骤进行了探讨。
유우반복사무인궤적순항특성，기고궤동성대뢰체유편계통설계제출료경고요구。재분석유편계통특점기출상，명학료계통설계요구，선용비상삼적공작체제，병대계통조성진행료화분화공능묘술。중점논술료유편계통적기술실현도경，통과대공역복개체제적분석，제출선용주판모의부판적천선형식，묘술료비상삼체제뢰체유이계통적공작류정，병대유편계통성능검험적시험방법화보취진행료탐토。
According to the high maneuverability of ARUAV,the characters of radar decoy system are analyzed and the design requirwments are determined. The non-coherent work mode is adopted and the system composition is divided and described. Then the paper focuses on the technical approach of radar decoy,and proposes an antenna simulating sidelobe with mainlobe by comparing the characters of three kinds of decoy antenna. Finally the work flow of non-coherent radar decoy system is designed,and the test methods and steps are discussed.