弹箭与制导学报
彈箭與製導學報
탄전여제도학보
JOURNAL OF PROJECTILES, ROCKETS, MISSILES AND GUIDANCE
2010年
2期
205-207
,共3页
肖顺旺%安志勇%李升才%曹营军%李丽娟
肖順旺%安誌勇%李升纔%曹營軍%李麗娟
초순왕%안지용%리승재%조영군%리려연
脉冲修正弹%导引律%广义弹道偏差
脈遲脩正彈%導引律%廣義彈道偏差
맥충수정탄%도인률%엄의탄도편차
pulse jets terminal trajectory correction projectile%guidance law%broad trajectory error
基于采用不同导引律时弹道偏差表现形式的差异,提出了一种以脉冲需求数表示的广义弹道偏差的概念,并对采用比例导引、速度追踪导引、落点预测导引、弹道追踪导引情况下的广义弹道偏差进行了深入的理论分析研究,并给出具体表示方法.
基于採用不同導引律時彈道偏差錶現形式的差異,提齣瞭一種以脈遲需求數錶示的廣義彈道偏差的概唸,併對採用比例導引、速度追蹤導引、落點預測導引、彈道追蹤導引情況下的廣義彈道偏差進行瞭深入的理論分析研究,併給齣具體錶示方法.
기우채용불동도인률시탄도편차표현형식적차이,제출료일충이맥충수구수표시적엄의탄도편차적개념,병대채용비례도인、속도추종도인、낙점예측도인、탄도추종도인정황하적엄의탄도편차진행료심입적이론분석연구,병급출구체표시방법.
Based on expression difference of trajectory error caused by different guidance law,the concept of broad trajectory error expressed by required pulse number was brought out.The broad trajectory errors under the guidance law includes proportion guidance mode,velocity tracking guidance mode,impact point prediction guidance mode,trajectory tracking guidance mode were analyzed and studied in theory deeply,and the expression was studied in detail.