飞控/惯导综合系统MIRA最优冗余结构设计
비공/관도종합계통MIRA최우용여결구설계
The Design of the Optimal Redundant Structure for the Flight-Control/Inertial Integrated System MIRA and the Research for Redundancy Management
  • 万方数据
    弹箭与制导学报 탄전여제도학보
    JOURNAL OF PROJECTILES, ROCKETS, MISSILES AND GUIDANCE
    2003年 1期 21-23 ,共3页

    张京妹%高社生%郭富强

    장경매%고사생%곽부강

    MIRA%故障检测与识别%最优结构 MIRA%故障檢測與識彆%最優結構
    MIRA%고장검측여식별%최우결구
    根据冗余度确定的原则,推导出了飞控/惯导综合系统MIRA最优冗余结构设计的基本条件-结构矩阵必须满秩;进而对结构矩阵的最优结构设计做了详细的推证.
    근거용여도학정적원칙,추도출료비공/관도종합계통MIRA최우용여결구설계적기본조건-결구구진필수만질;진이대결구구진적최우결구설계주료상세적추증.
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