首页 | 官方网站   微博 | 高级检索  
     

压电捷联惯导系统研究
引用本文:赵忠.压电捷联惯导系统研究[J].压电与声光,2000,22(2):78-80.
作者姓名:赵忠
作者单位:西北工业大学,自动控制系,西安,710072
基金项目:国防基金资助项目!(98J9. 2. 6. HK0308,99J9. 2. 4. HK0305)
摘    要:探讨了用压电惯性器件构筑捷联惯导系统的技术途径。叙述了压电捷联惯导系统的结构及特点,分析并指出了惯性器件及系统的主要误差源,为压电陀螺和压电加速度计提出了一种系统级综合校正模型.给出了基于四元数的姿态及导航实时算法,对校正后的系统性能进行了仿真计算。结果表明,压电捷联惯导系统精度可以满足一些领域的导航与制导要求。对原理样机所做初步试验得到的结果优于仿真精度。

关 键 词:陀螺  加速度计  捷联惯导系数  导弹  制导方式
修稿时间:1999-12-28

Strapdown Inertial Guidance System Consi sting of Piezoelectric Inertial Sensors
ZHAO Zhong.Strapdown Inertial Guidance System Consi sting of Piezoelectric Inertial Sensors[J].Piezoelectrics & Acoustooptics,2000,22(2):78-80.
Authors:ZHAO Zhong
Abstract:The technical w ay to build inertial guidance system wit h piezoelectric inertial sensors is disc ussed and this strapdown system has the typical performances of low cost,miniatu re dimension,high reliability,DC power a nd low energy consumptionMain errors in  the inertial elements and in the system  are analyzed and pointed outThe system -level correction models both for piezoe lectric gyroscope and for piezoelectric accelerometer are presentedThe real-tim e attitude and navigation algorithms bas ed on quaternions are givenComputer sim ulation results show that the accuracy o f the system calibrated satisfies the gu idance and navigation requirements of so me vehiclesThe real accuracy of a proto type system gained from elementary exper iments is much better than the simulated
Keywords:gyroscope  accelerometer  strapdown inertial guidance system  algorithm  
本文献已被 CNKI 维普 万方数据 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-23

京公网安备 11010802026262号