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《Tactical Missile Technology》 1996-02
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STUDY ON DYNAMIC AZIMUTH ALIGNMENT TECHNOLOGY OF SINS FOR SHIPBOARD MISSILE

Li lixin The Third Research Academy of CASC  
The dynamic alignment principle and mathematic model that uses angle rate matching is given. Aimming at the direct azimuth alignment problem of SINS for shipboard missile,the technology using indi- rect azimuth alignment of local reference is presented.Shaking test and shipboard test show that this technol- ogy can increase the precision and quick-acting of azimuth alignment.
【CateGory Index】: TJ762.3
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【References】
Chinese Journal Full-text Database 4 Hits
1 Fang Xin-hu;Lin Song;Zhang Qian;Zhai Zhang-ming;China Academy of Launch Vehicle Technology;Beijing Institute of Aerospace Systems Engineering;;Study of Moving-base Aiming Applied on Submarine-launched Missile[J];导弹与航天运载技术;2015-02
2 Yang Haibo1,Gao Guanglin2,Wang Ruichen1(1.Navy Submarine Academy,Qingdao,266071;2.Tianjin Campus,Naval University of Engineering,Tianjin,300450);Inertial Navigation System Rapid Initial Alignment Concept on Moving Base[J];导弹与航天运载技术;2010-05
3 Yang Haibo,Hong Zhenqi,Ma Xuan(Navy Submarine Academy,Qingdao 266071,China);Study of the Project of Quick Horizontal Adjusting and Compensating of SINS Platform in Submarine-launched Missile[J];战术导弹技术;2010-04
4 YANG Hai-bo,HONG Zhen-qi,ZHU Feng-qi (Navy Submarine Academy,PLA,Qingdao 266071,China);The Accuracy Analysis and Assessment of the Sighting Method of a Submarine-Launched Missile[J];火力与指挥控制;2009-06
【Co-references】
Chinese Journal Full-text Database 5 Hits
1 LV-Wei YAN Yang-Dong WANG Li-na 1 Beijing University of Aeronautics and Astronautics,Beijing 100083,China 2 The Second System Design Department of the Second Research Academy of China Aerospace Corporation,Beijing 100854,China);A Study on SINS Rapid Alignment Technology On Moving Base[J];弹箭与制导学报;2005-SA
2 LEI Xu-liang,SONG Jin-lai,ZHOU Yi-lan(The Academy of China Aerospace Times Electronic Corporation,Beijing 100854,China);Fast Initial Alignment for Strapdown Inertial Navigation System[J];中国惯性技术学报;2005-04
3 CHEN Xin-min~1,XIE Quan-gen~2 (Beijing Institute of Astronautical Systems Engineering,Beijing 100076);Study of composite guidance applicable to launch vehicles[J];宇航学报;2004-03
4 Li lixin The Third Research Academy of CASC;STUDY ON DYNAMIC AZIMUTH ALIGNMENT TECHNOLOGY OF SINS FOR SHIPBOARD MISSILE[J];战术导弹技术;1996-02
5 Li Lixin The Third Research Academy of CASC;STUDY OF DYNAMIC INITIAL ALIGNMENT TEST USING VELOCITY MATCHING[J];战术导弹技术;1994-03
【Secondary References】
Chinese Journal Full-text Database 5 Hits
1 LU Wenzhong;LIU Bingjie;JI Haiyan;Navy Submarine Academy;;Missile Platform Shifting Process Model Identification Based on Support Vector Regression[J];弹箭与制导学报;2014-02
2 WANG Xiao-qiang;JIA He-ming;China Airborne Missile Academy;College of Mechanical and Electrical Engineering, Northeast Forestry University;;Fast Alignment Method in Moving Base for SINS[J];自动化技术与应用;2013-11
3 WANG Li-dong,LIU Jun,LU Jun(Ordnance Engineering College,Shijiazhuang 050003,Hebei,China);Coning Error Compensation Algorithm of SINS Self-Alignment on Swaying Base[J];兵工学报;2012-07
4 HE Bing,LIU Gang,LEI Gang,WANG Yuan-yuan(№9 Department,The Secondary Artillery Engineering College,Xi’an 710025,China);Computing and Simulation Analysis of Flight Envelope of Cruise Missile[J];海军航空工程学院学报;2011-06
5 HE Bing,LIU Gang,LEI Gang,WANG Yuanyuan(The Second Artillery Engineering College,Xi'an,Shaanxi Province 710025);Research on Factors of Influence on Cruise Missile Flight Envelope[J];飞行器测控学报;2011-02
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