搜索资源列表
Simulation-of-SINS
- 捷联惯导仿真，对于初学惯导的人进行matlab仿真有很大的帮助！-Simulation of SINS
initial_track
- 惯导轨迹仿真，对于初学惯导的人有很大的帮助-INS trajectory simulation, inertial navigation for beginners who have a lot of help
SINS
- 捷联惯导仿真，对于初学捷联惯导的人有很大的帮助-SINS simulation SINS for the beginner who has a lot of help
SINS
- 指北方位捷联惯导解算。。。尽管下吧，写作业的时候会用到-SINS navigation code
Yan-Gong-Min-_-PhD-thesis
- 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
postdoctor-research-report
- 严恭敏博士后研究工作报告——捷联惯导系统动基座初始对准及其它相关问题研究报告 内容包括：大失准角下捷联惯导系统动基座初始对准，激光陀螺整周期采样对姿态解算的影响极其修正方法。SINS内杆臂效应分析与补偿，圆锥误差补偿。-Yan Gong Min postdoctoral research report- Moving Base SINS initial alignment study and other related issues Content includes: Large Mis
main
- 利用参数辨识法提取相关对准参数，从而估计出陀螺漂移和数学平台偏角并进行补偿。仿真结果表明，开路罗经法对准具有较高的对准精度、较好的快速性，能够满足捷联惯导系统在静基座下实现自对准的要求。-Expressions of mathematical platform misalignment angles of the open-loop algorithm are derived and parameter identification method is used to pick-up the
navigation
- navigation.rar包含5个有用的导航程序； navigation.m为纯惯导解算程序； integrated_navigation为组合导航程序； KalmanAlign10.m为卡尔曼滤波对准程序； create_data.m为原始数据创建程序； ssm.m为结果显示程序-navigation.rar contains five useful navigation program navigation.m pure INS solver KalmanAl
SINS-MATLAB
- matlab 编写的惯导定位程序，可以直接运行-INS positioning written in matlab program can be run directly
fault-detection
- 实现了以惯导为基准的组合导航系统，完成了组合导航系统的故障诊断-Achieved with a combination of inertial-based navigation system, the completion of the integrated navigation system fault diagnosis
test2
- 基于基础卡尔曼滤波的捷联惯导系统初始对准，精对准，静基座。-Based on SINS initial alignment-based Kalman filter, fine alignment, static base.
openloop_kalman_velocity
- 利用惯导和GPS定位解算出的速度和位置进行卡尔曼滤波，对惯导的输出参数进行校正。-GPS positioning using the inertial velocity and the calculated position solution and the Kalman filter, the output parameters of the INS to be corrected.
INS5
- 惯导姿态解算，根据加速度计和陀螺的测量数值，求解惯导系统的姿态，速度和位置的代码-INS attitude solution
main007(Kalman)--
- 惯导系统C语言程序，使用卡尔曼进行滤波，四元数更新姿态矩阵-Inertial Navigation System C language program, using the Kalman filter, quaternion attitude matrix update
INS_static
- 惯导静基座解算程序(考虑陀螺和加速度计的随机常值误差和白噪声）-Inertial navigation system on static basis
INS_active
- 惯导系统动基座下的解算过程（包含轨迹生成器和导航解算，器件只考虑随机常值误差和白噪声）-INS on active basis
bsgui2
- 平台惯导的误差分析，及误差补偿，并在多种轨迹下进行了仿真-INS error analysis and error compensation, and in a variety of trajectories simulated
lowpassfilter
- 在捷联惯导初始对准中，由于偏航角的误差较大，对准速度较慢，增加了低通滤波器，并通过横滚角和俯仰角来加快对准速度-In SINS initial alignment, the error of yaw angle, aligning slower, increasing the low-pass filter, and through the roll angle and pitch angle to accelerate the speed of the alignment
kalmaninitialize
- 利用GPS和SINS组合来对捷联惯导初始对准进行仿真，效果较好-Use a combination of GPS and SINS SINS initial alignment for the simulation, better
INS_ours
- 惯性导航，此为基于四元素法，角增量法的捷连惯导系统程序算法-Inertial navigation, this is based on four elements, and angular increments law Jie Lian INS program algorithm