宇航计测技术
宇航計測技術
우항계측기술
JOURNAL OF ASTRONAUTIC METROLOGY AND MEASUREMENT
2014年
6期
14-18,13
,共6页
捷联惯导%快速传递对准%卡尔曼滤波
捷聯慣導%快速傳遞對準%卡爾曼濾波
첩련관도%쾌속전체대준%잡이만려파
SINS%Rapid transfer alignment%Kalman filter
为了研究海况与航母机动方式对舰载机捷联惯导快速传递对准的影响,以姿态误差角为研究对象,建立了惯导系统的比力方程和姿态微分方程。从误差传播机理出发,详细推导了速度匹配和速度加姿态匹配的误差模型,然后用卡尔曼滤波算法进行仿真分析。仿真结果表明,航母有一定摇摆幅度更有利于舰载机进行速度匹配或速度加姿态匹配;典型海况条件下,航母的机动方式对速度匹配传递对准方式影响较为明显。
為瞭研究海況與航母機動方式對艦載機捷聯慣導快速傳遞對準的影響,以姿態誤差角為研究對象,建立瞭慣導繫統的比力方程和姿態微分方程。從誤差傳播機理齣髮,詳細推導瞭速度匹配和速度加姿態匹配的誤差模型,然後用卡爾曼濾波算法進行倣真分析。倣真結果錶明,航母有一定搖襬幅度更有利于艦載機進行速度匹配或速度加姿態匹配;典型海況條件下,航母的機動方式對速度匹配傳遞對準方式影響較為明顯。
위료연구해황여항모궤동방식대함재궤첩련관도쾌속전체대준적영향,이자태오차각위연구대상,건립료관도계통적비력방정화자태미분방정。종오차전파궤리출발,상세추도료속도필배화속도가자태필배적오차모형,연후용잡이만려파산법진행방진분석。방진결과표명,항모유일정요파폭도경유리우함재궤진행속도필배혹속도가자태필배;전형해황조건하,항모적궤동방식대속도필배전체대준방식영향교위명현。
In order to study the Way hoW the sea conditions and the carrier mobility affect on carri—er—based aircraft SINSˊrapid transfer alignment, using the attitude error angle as research object, a specific force equation and attitude differential equation of inertial navigation system are established. The error model of velocity matching and velocity plus attitude matching are deduced detailly based on error propagation mechanism. Then simulating and analyzing are carried out With Kalman filter algorithm. The simulation results shoW, a certain sWing amplitude is more conducive to aircraft, s velocity matching or velocity plus attitude matching. Under typical sea conditions, the velocity matching transfer alignment is affected more obviously by aircraft carrier, s line motion.