首页 | 本学科首页   官方微博 | 高级检索  
     检索      

弹道导弹GPS/SINS组合制导品质控制研究
引用本文:王永刚,袁建平.弹道导弹GPS/SINS组合制导品质控制研究[J].飞行力学,1997,15(1):91-96.
作者姓名:王永刚  袁建平
作者单位:西北工业大学!西安,710072
摘    要:给出了可提高战术弹道导弹射击精度的GPS/SINS组合制导模型。在给出多模Kalman滤波(MKF)数学模型的基础上和建立了可对GPS/SINS组合制导进行在线故障检测,故障了和系统重构的品质控制方案对于系统的重构,提出了鲁棒性处理方法。仿真结果表明:基于MKF的GPS/SINS组合制地与单独捷联惯导相比,可使导弹射击精度和到明显提高,组合地的品质也得到了有效控制。

关 键 词:GPS  组合制导  弹道导弹

Ballistic Missile GPS/SINS Integrated Guidance Quality Control
Wang Yonggang,Yuan Jianping,Chen Shilu.Ballistic Missile GPS/SINS Integrated Guidance Quality Control[J].Flight Dynamics,1997,15(1):91-96.
Authors:Wang Yonggang  Yuan Jianping  Chen Shilu
Institution:Northwestern Polytechnical University
Abstract:A BPS/SINS integrated guidance model which can raise tactical ballistical missile (TBM) impact accuracy is given. Be rs d on multimode Kalman filter (MKF) models, an integrated guidance quality control approach which can be simultaneously used to detect, isolate TBM BPS/SINS system failure and reconstruct integrated system, is introduced. We also proposed robust ways to reconstruct system. The imitation results show that compared with single SIMU guidance system, GPS/SINS system based on MKF can clearly raise impact accuracy, and guidance cluality can also be effectivelly controled.
Keywords:Kalman filter  Global Positioning System (GPS)  Integrated Guidance  Quality control
本文献已被 CNKI 维普 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号