战术弹道导弹SINS/GNSS/SAR组合制导方法研究  

Study of Tactical Ballistic Missile with Integrated Guidance System SINS/GNSS/SAR

作　　者：张君昌[1] 侯义斌[1] 邹维宝[2] 高社生[2] 

机构地区：[1]西安交通大学工程院,西安710049 [2]西北工业大学自动控制系,西安710072

出　　处：《弹箭与制导学报》2000年第4期38-41,56,共5页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：针对 SINS/GPS组合制导系统在战术弹道导弹的应用中存在的问题 ,本文在该组合系统中融入了合成孔径雷达 (SAR)传感器 ,用以提高系统的自主性、容错性和制导精度。仿真结果表明 ,SINS/GNSS/SAR组合系统的制导精度比SINS/GPS有所提高。For the problem of SINS/GPS integrated guidance system, this paper fuses a sensor of synthetic aperture radar(SAR) with it to improve its independence, fault tolerance and guidance precision. The simulation results prove that SINS/GNSS/SAR's guidance precision has been improved compared to INS/GPS's. So INS/GNSS/SAR integrated guidance system is of high performance.

关 键 词：SINS/GPS 组合制导系统 SINS/GNSS/SAR 战术弹道导弹 

分 类 号：TJ761.3[兵器科学与技术—武器系统与运用工程] TJ765.3