Description: Kalman滤波器，卡尔曼滤波器算法说明及其实现。C语言编写的函数，可以直接调用。-Kalman filter, the Kalman filter algorithm note and its realization. C language function can be called directly. Platform: |
Size: 3072 |
Author:周国翔 |
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Description: 利用三轴角速率型号和三轴加速度计信号结合扩展卡尔曼滤波实现三个姿态角度的融合-The use of three-axis angular velocity model and three-axis accelerometer signal extended Kalman filter combined with the realization of the integration of the three attitude angles Platform: |
Size: 2150400 |
Author:张晓坤 |
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Description: 实现GPS+IMU扩展卡尔曼滤波组合导航，重力场和磁场推算姿态-Achieve the GPS+ IMU extended Kalman filter integrated navigation, gravity field and magnetic field profile projection Platform: |
Size: 274432 |
Author:张坤 |
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Description: 对基于弹载IMU/C:PS组合导航系统的动基座对准问题进行了研究与仿真 首先，分析了弹载IMU与GI S的系统误差，建立获得了其系统误差模型 然后，利用卡尔曼滤波技术，设计了弹载IMU/UPS组合导航系统的动基座对准算法 -Based on onboard IMU/C: PS Integrated Navigation System Alignment conducted a study and simulation first analyzed onboard IMU and GI S of the system error, the establishment of the system error model obtained and then, using Kalman filter technology, designed Missile IMU/UPS Integrated Navigation System Alignment Algorithm Platform: |
Size: 2029568 |
Author:song |
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Description: 对基于弹载IMU/C:PS组合导航系统的动基座对准问题进行了研究与仿真 首先，分析了弹载IMU与GI S的系统误差，建立获得了其系统误差模型 然后，利用卡尔曼滤波技术，设计了弹载IMU/UPS组合导航系统的动基座对准算法 -Based on onboard IMU/C: PS Integrated Navigation System Alignment conducted a study and simulation first analyzed onboard IMU and GI S of the system error, the establishment of the system error model obtained and then, using Kalman filter technology, designed Missile IMU/UPS Integrated Navigation System Alignment Algorithm Platform: |
Size: 1875968 |
Author:song |
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Description: 对基于弹载IMU/C:PS组合导航系统的动基座对准问题进行了研究与仿真 首先，分析了弹载IMU与GI S的系统误差，建立获得了其系统误差模型 然后，利用卡尔曼滤波技术，设计了弹载IMU/UPS组合导航系统的动基座对准算法 -Based on onboard IMU/C: PS Integrated Navigation System Alignment conducted a study and simulation first analyzed onboard IMU and GI S of the system error, the establishment of the system error model obtained and then, using Kalman filter technology, designed Missile IMU/UPS Integrated Navigation System Alignment Algorithm Platform: |
Size: 3579904 |
Author:song |
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Description: 针对IMU和GPS联合解算提供了两个不同的卡尔曼滤波算法-IMU and GPS for the United Solution offers two different Kalman filter Platform: |
Size: 20480 |
Author:向华强 |
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Description: The open source project DSP_INS is an inertial navigation system on the TI DSP
platform TMS320F28335 with MEMS inertial sensors and commercial GPS module. Inertial
sensors are actually used only for estimating attitude, heading and velocity.
Position information totally comes from GPS (see Q2 in FAQ part). Currently the
MEMS IMU (Inertial Measurement Unit) ADIS16355 and GPS module u-blox LEA-5H
are supported. DSP_INS also reads magnetic field data from HONEYWELL HMC1051/1052.
You can also use the latest IMU module ADIS16405, which also contains magnetic field
sensors.
There is a 10-order extended Kalman filter in DSP_INS, which takes angular velocity,
acceleration, magnetic field, and GPS velocity as inputs. It provides outputs
including angular velocity, acceleration, attitude, heading, velocity, and position
(from GPS) every 10 milliseconds. DSP_INS is proved to be effective and reliable in
several robot and UAV projects. Platform: |
Size: 1682432 |
Author:snthej |
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Description: 很好的GPS/INS超紧组合导航的文章，关键词：GPS,INS，超紧组合导航，抗干扰-The performance of an Ultra-Tightly Coupled
(UTC) Global Positioning System/Inertial Navigation System
(GPS/INS) is evaluated using a system simulation of the GPS
receiver and navigation processing. The UTC system being
analyzed uses a bank of pre-filters to estimate code delay error
and Doppler frequency error for each satellite. These outputs are
sent to a central Kalman navigation filter. This central processor
generates estimates of inertial navigation position, velocity, and
attitude errors IMU biases and user clock errors, which are
used to correct the navigation solution. In the UTC approach,
outputs from the central navigation processor, after projection
into satellite line-of-sight coordinates, are used to control the
code and carrier replica signals for each satellite channel. In
contrast, a conventional tightly coupled GPS/INS system uses
separate tracking loops for each satellite channel, which operate
autonomously. As a result, the UTC desig Platform: |
Size: 461824 |
Author:lili |
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Description: 实现GPS+IMU扩展卡尔曼滤波组合导航，重力场和磁场推算姿态-Achieve the GPS+ IMU extended Kalman filter integrated navigation, gravity field and magnetic field profile projection Platform: |
Size: 10770432 |
Author:黄小法 |
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Description: 无迹卡尔曼滤波模型，具有详细注释，可修改为自己合适模型(Unscented Kalman filter model, with detailed notes, can be modified to its own appropriate model) Platform: |
Size: 56320 |
Author:wong11264 |
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Description: In this assignment you will study an inertial navigation system (INS) constructed using sensor fusion by a Kalman filter. The start code provides you with a working system with an inertial measurement unit (IMU, here accelerometer+gyro) and GNSS (GPS). Platform: |
Size: 195680 |
Author:ervaskes.pcet@gmail.com |
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