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program
- 较为复杂的捷联惯导导航，加入了姿态、位置、位置、速率信息。-SINS more complex navigation, joined the attitude, position, position, velocity information.
another
- 复杂捷联惯导的另一种解算方法，包括解算位置、速率与姿态-Complex SINS another solution method, including calculating position, velocity and attitude
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
SimulationSINS
- 基于四元数法的捷联惯导系统仿真，陀螺仪和加速度计数据为自己仿的一分钟数据-Simulation 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
SINS-MATLAB
- 捷联惯导（SINS）的MATLAB仿真程序-SINS of the MATLAB simulation program
ceziwucha
- 这是捷联惯导系统一阶、二阶微分方程法和一阶、二阶四元数法和完整解之间的误差代码-This is the sins of the first order, second order differential equation method and first order, second order quaternion method and the error between the full code solution
siyuanshu
- 捷联惯导 四元数法 进行导航姿态解算 程序内有详细注解-SINS quaternion attitude solver for navigation with detailed comments
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
56356291j
- 捷联惯导程序,利用matlab编写的程序，很有参考价值-SINS SINS program program program SINS ，using matlab language，
Attitude-SINS
- 姿态角仿真 MATLAB 捷联惯导 三阶泰勒 四阶龙格库塔-MATLAB simulation Attitude SINS fourth order Runge-Kutta third-order Taylor
wc
- 分析初始对准误差，随机误差对捷联惯导精度的影响-Analysis of initial alignment errors, random errors on the precision of SINS
jlgd
- 自编的捷联惯导程序，四元素的初值及更新、速度和位置的更新及解算-Self SINS program, the four elements of the initial and updated velocity and position updates and the Solution
nonlinear-alignment-method
- 捷联惯导四元数误差模型，采用ukf作为滤波方法。-nonlinear alignment method for sins
integrated-navigation
- 组合导航kalman滤波程序 自己写的 包括采集的数据初始对准以及捷联解算等程序-Kalman filter combined navigation program himself wrote of the data collected include initial alignment and strapdown computation programs
a-new-method-for-moving-SINS
- 本文在运载体运动情况下，提出了一种适用于捷联惯导系初始对准的新算法，该算法以 惯性空间为参考基准，将初始对准姿态矩阵的实现分解为三部分-This movement of the transporter, the paper presents a system for SINS Initial Alignment of the new algorithm to inertial space as the reference point, the realization of initial a
Track_S
- 导航四元素法捷联惯导的四元素算法捷联惯导的四元素简单算法-strapdown inertia navigation
main
- matalab仿真的捷联惯导，写的比较清楚明白(Strapdown inertial navigation system based on MATALAB simulation)
strapdown
- 捷联惯性导航数据分析，很基础的程序代码，有助于初学者理解(Strapdown inertial navigation data analysis)