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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 inertialguidance system wit h piezoelectric inertial sensors is disc ussed and this strapdownsystem 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 thesystem  are analyzed and pointed outThe system -level correction models both for piezoelectric gyroscope and for piezoelectric accelerometer are presentedThe real-tim e attitude and navigation algorithms bas edon quaternions are givenComputer sim ulation results show that the accuracy o f the system calibratedsatisfies the gu idance and navigation requirements of so me vehiclesThe real accuracy of a proto type system gained fromelementary exper iments is much better than the simulated
Keywords:gyroscope  accelerometer  strapdown inertial guidance system  algorithm  
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