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INS 平台式惯性导航系统仿真
- 平台式惯性导航系统仿真，可用于学习误差分析，静基座卡尔曼滤波对准-Platform inertial navigation system simulation,can be used to study error analysis ，the static Kalman filter aligned base
chzf.rar
- 惯性导航系统中求解航向及姿态角的仿真程序，用matlab开发,Inertial navigation system to solve direction and attitude angle of the simulation program, developed by matlab
Navigater_programmer.rar
- 一个机器小车的组合导航系统，GPS+惯性导航，内有DSP和FPGA的程序，比较完整,A combination of a machine car navigation system, GPS+ inertial navigation, which has DSP and FPGA program
transfer
- 惯性导航系统传递对准系统模型程序，请大侠诚恳指教，多谢-Inertial navigation system alignment system model transfer process, please sincerely advice heroes, I would like to thank
kal(VC++)
- 用vc来写的卡尔曼滤波程序实现了车辆惯性导航系统的卡尔曼滤波，包括定位结算，姿态校正，速度校正等-Vc to write with Kalman filtering process to achieve a vehicle inertial navigation system of the Kalman filter, including the positioning settlement, posture correction, the speed of correction
796e50c2-1775-4730-8213-2225004ca5c1
- 利用matlab数值计算的强大功能和,建模容易实现的特点"进行了捷联式惯性导航系统的仿真研究,对四元数及姿态矩阵等的解算采用编程实现"陀螺仪和加速计的建模用.-Matlab numerical calculation using the power and, modeling the characteristics of easy to implement " a strapdown inertial navigation system of the simulation study a
navigationsys
- 惯性导航系统仿真试验研究及其详细的编程实现方法-Inertial navigation system and its simulation programming
INSGPS
- 本文介绍了GPS和工NS的基本原理和组成，建立了组合导航系统误差模型，推导了 惯性导航系统误差方程，主要研究了INS/GPs组合导航中卡尔曼滤波技术的应用问题。-This thesis introduces basic principle and composition of GPS and INS， infers the system error equations，getstheerrormode，studiesaPPlicationof Kalman filtering in
87361024AFastInitialAlignmentMethodofInertialNavig
- 捷联惯性导航系统的初始对准，程序。组合导航程序-inertial navigation alignment
SINS_Kalman
- 捷联惯性导航系统、GPS/SINS组合导航系统仿真程序-Strapdown inertial navigation systems, GPS/SINS Integrated Navigation System Simulation Program
GPSSINS
- GPS与惯性导航系统组成的组合导航系统仿真程序-GPS and inertial navigation system consisting of integrated navigation system simulation program
toolofINS
- 惯性导航系统工具箱 能有效帮助仿真惯性导航系统-Inertial navigation system simulation toolbox can be effective in helping inertial navigation system
EKFsins
- 捷联惯性导航系统的卡尔曼滤波对准程序，非常有用-alignment sins
EKF_5order
- EKF在捷联惯性导航系统初始对准中的应用？在方位角为大失准角的情况下，如何进行初始对准-EKF in SINS Initial Alignment? In the azimuth misalignment angle for the big cases, how to initial alignment
NEW
- 基于四元数法的捷联惯性导航系统姿态解算及正弦输入函数的生成-Quaternion-based strapdown inertial navigation system attitude solution and the generation of sinusoidal input function
simulation
- MATLAB_Simulink的捷联惯性导航系统仿真-MATLAB_Simulink of strapdown inertial navigation system simulation
51622443trace_generate
- c语言编写的惯性导航系统轨迹发生器，用于结算惯性导航系统(inertial navigation system)
Factor Graph in Inertial Navigation Systems
- 利用因子图和积算法设计的无人机惯性导航系统算法，利用matlab仿真实现(An algorithm of unmanned aerial vehicle (UAV) inertial navigation system designed by factor diagram and calculation method is realized by MATLAB simulation)
高精度捷联惯性导航系统Matlab工具箱
- 工具箱主要功能: 1） 姿态向量、四元数、矩阵、滤波算法等各类子程序 2） 圆锥运动仿真 划船运动仿真 惯性器件随机误差仿真 3） Kalman滤波初始对准 基于惯性系初始对准 罗经法初始对准 大方位失准角EKF初始对准 大失准角UKF初始对准 速度+姿态传递对准 4） 纯惯性导航SINS仿真 航位推算、SINS/DR仿真 SINS/GPS组合仿真 GPS/BD/GLONASS单点伪距定位 SINS/GPS松/紧组合 POS正逆向数据处理与信息融合仿真 5）((Toolbox main func
crazyfile
- 捷联式惯性导航系统姿态结算，可以得出pitch（y轴）和roll（x轴） 方案为：stm32+mcu6050(Inertial navigation system attitude settlement can be drawn pitch (y-axis) and roll (x-axis) Solutions for: stm32+ mcu6050)