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Nassar - Improving the Inertial Navigation System INS Error Model for INS and INS-DGPS-Nassar- Improving the Inertial Navigation System INS Error Model for INS and INS-DGPS
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An old but important paper in IEEE about two different approaches of inertial navigation system error modeling. it is not available in "IEEE Xplore", but I converted it from microfilm to PDF.
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基于光学陀螺惯导系统的误差自动补偿技术Based on optical gyroscope inertial navigation system with automatic error compensation technology-Based on optical gyroscope inertial navigation system with automatic error compensation technology
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随着GPS性能的不断完善，应用越来越广泛，但GPS系统易受到外界环境影响，而传统的惯导系统也具有误差随时间积累的缺陷，因此GPS/INS组合方式因其互补性强已经成为实现导航的重要方式。这种组合方式能够确保在采用较廉价的惯性设备的情况下，也能获得较好的导航效果。-With the constant improvement of the GPS performance, more and more widely, but the GPS system vulnerable to external e
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严恭敏_博士学位论文
论文中采用激光陀螺捷联惯导系统为主导航系统，通过与里程计和气压高度计组合，构成车载自主定位定向系统，并借助路标点进行误差补偿。该定位定向系统不依靠 GPS，中途无须停车作零速修正，是一种全自主的导航系统，具有定位定向精度高、机动性好、可靠性高和寿命长等优点。 -In this thesis, laser gyro strapdown inertial navigation system (SINS)
is selected as core navigation s
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