搜索资源列表
DNS
- 用DSP实现的光纤捷联惯导系统DSP implementation of the optical fiber with SINS-DSP implementation of the optical fiber with SINS
matlab
- 捷联惯性导航的卡尔曼滤波 初始对准程序-SINS initial alignment procedure of Kalman filtering
locus
- 捷联惯导的轨迹发生器，matlab版本，生成比力，角速度等信息-SINS trajectory generator, matlab version, generated more than force, angular velocity and other information
ourdev_430061
- 基于卡尔曼滤波的飞行器姿态控制，包括估计模块和控制算法模块-Based on Kalman Filtering for Spacecraft Attitude Control, including the estimation module and the control algorithm module
gpsins
- 姿态解算程序，用于捷联惯导系统的姿态解析算法-Attitude solution procedures for the sins of attitude analytic method
gorithm
- 捷联惯导系统姿态测量算法SINS attitude determination algorithm-SINS attitude determination algorithm
1
- 体系相对导航系的角速度在体系上的分量 参照捷联惯性_里程仪_伪卫星车载组合导航系统研究 locity(i,:)) ) - gn 车体相对惯性系加速度在地理坐标系上的分量，标称值 参照捷联惯性_里程仪_伪卫星车载组合导航系统研究36 --两个论文-System angular velocity relative navigation system' s components in the system, inertial reference _ OD _ Pseudo Satelli
123
- 体系相对导航系的角速度在体系上的分量 参照捷联惯性_里程仪_伪卫星车载组合导航系统研究 locity(i,:)) ) - gn 车体相对惯性系加速度在地理坐标系上的分量，标称值 参照捷联惯性_里程仪_伪卫星车载组合导航系统研究36 --1个论文（GPS中频信号处理及其FPGA实现）-System angular velocity relative navigation system' s components in the system, inertial reference _
SINS-Alignment(matlab)
- 捷联惯导初始对准的程序 matlab写的 包括动基座和静基座对准。-Initial Alignment of SINS program written in matlab, including dynamic and static alignment.
MATLAB-sins
- 利用matlab编写的捷联惯导程序，可以做参考，参考价值大-Prepared using matlab SINS program, you can do reference, reference-value
strapdown
- 捷联惯导源程序，matlab编写 捷联惯导源程序，matlab编写-SINS source code, matlab write SINS source, matlab write
strapdown
- 对捷联惯导的速度、经纬度、姿态角等参数进行解算-A programme to compute the speed,latitude,longitude and attitude of strapdown inertial navigation system
INS_navigation
- 导航 惯性 自主 捷联 近地 惯性 导航-navigation autonomous
trajectory
- 捷联惯导中的模拟轨迹程序，适用于惯导学习者-SINS trajectory
A-New-GPS-Aided--Initial-for-SINS
- 本文针对捷联惯导系统(SINS)初始对准问题,提出了一种无需经历传统的粗对准阶段而利用单天线GPS辅助直接进行动基座精确初始对准的新方法 -In this paper, SINS (SINS) initial alignment problem, we propose a coarse alignment without experiencing the traditional stages of a single-antenna GPS-assisted direct precise mo
SY0917207_ChuYanlong_GD_2
- 惯导捷联式平台的应用，通过此平台来仿真计算星体的位置，各种姿态。-INS strapdown platform applications, simulation through this platform to the position of the stars, the various postures.
Ekf_filter2
- 捷联惯性导航的扩展卡尔曼滤波的算法，非常好用的算法-Strapdown initial navigation
jielian
- 捷联惯导航姿系统C语言实现，可以方便的得到飞机的飞行姿态。-Navigation position system SIMU program development, you can easily get the aircraft attitude.
Kalman
- 捷联惯导初始对准Kalman滤程序，非常难得的代码源程序。-SINS initial alignment Kalman filter program, source code is very rare.
navi_test
- 用四元数法的捷联惯性导航姿态解算程序。可以快速准确得到数据。-With the quaternion method Inertial attitude solver. You can get fast and accurate data.