宇航学报
宇航學報
우항학보
JOURNAL OF ASTRONAUTICS
2010年
2期
404-409
,共6页
徐军辉%郑玉航%汪立新%易昭湘
徐軍輝%鄭玉航%汪立新%易昭湘
서군휘%정옥항%왕립신%역소상
捷联惯组%射前标定%补偿修正%落点精度%弹道仿真
捷聯慣組%射前標定%補償脩正%落點精度%彈道倣真
첩련관조%사전표정%보상수정%낙점정도%탄도방진
Strapdown inertial measurement unit%Pre-launching%Compensation and amendment%Landing accuracy%Ballistic emulation
针对导弹武器捷联惯组使用精度不高的问题,提出了通过射前标定和误差系数补偿修正技术来提高其使用精度.不借助任何外部工具,完全依靠导弹自身提供的信息,射前标定11个误差系数,利用单次通电特性及等效补偿和落点偏差二次修正技术来减小落点偏差.弹道仿真结果表明,射前标定方法结合误差系数补偿修正技术能够有效地提高导弹的命中精度.
針對導彈武器捷聯慣組使用精度不高的問題,提齣瞭通過射前標定和誤差繫數補償脩正技術來提高其使用精度.不藉助任何外部工具,完全依靠導彈自身提供的信息,射前標定11箇誤差繫數,利用單次通電特性及等效補償和落點偏差二次脩正技術來減小落點偏差.彈道倣真結果錶明,射前標定方法結閤誤差繫數補償脩正技術能夠有效地提高導彈的命中精度.
침대도탄무기첩련관조사용정도불고적문제,제출료통과사전표정화오차계수보상수정기술래제고기사용정도.불차조임하외부공구,완전의고도탄자신제공적신식,사전표정11개오차계수,이용단차통전특성급등효보상화낙점편차이차수정기술래감소낙점편차.탄도방진결과표명,사전표정방법결합오차계수보상수정기술능구유효지제고도탄적명중정도.
Aiming at the performance accuracy problem of strapdown inertial measurement unit (SIMU), a method combined pre-launching calibration with error coefficient compensation and amendment technology was used to improve the performance accuracy. Depends on the information supplied by missile itself, 11 error coefficients can be calibrated before launching. Pre-launching compensation technique and quadric modification technique of landing error are introduced to reduce the landing error. The ballistic emulation results show that this method can effectively improve the hitting accuracy.