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strapdown
- 一篇确定捷联惯导初始姿态的专利文章,通过设置监控陀螺对其他三个陀螺进行测漂-A determined attitude SINS initial patent articles, by setting the monitor to the other three gyroscopes to measure gyro drift
trace
- 惯性导航精解算程序 C开发环境 Cdevelopment environment -Solver precision inertial navigation procedures C development environment Cdevelopment environment
ins
- 指北平台惯导导航系统的解算,导入比力,求得导航信息-navigation caculating for ins
INSandGPS
- 捷联惯导GPS组合导航Kalman滤波器-SINS GPS Navigation Kalman Filter
IMU7200
- 关于一个测试文档,主要是协议,关于惯导器件的一个,从网上下的,用16355测试,感觉还不错,就是有点漂,内容主要是关于IMU7200的一个装置的说明以及协议。-On a test document, the agreement is mainly on an inertial device, from the Internet under, with 16,355 tests, feeling good, that is, a litt
guider
- 进行惯导的代码,C语言;进行惯导的代码,C语言-For inertial navigation code, C language for inertial navigation code, C language
daohang
- 关于GPRS和惯导导航的仿真实验程序,是航空类的专业应用。好用-On the GPRS and the inertial navigation simulation program, the aviation class professional applications. Handy
SINS-SAR
- 捷联惯导和合成孔径雷达组合导航程序,地理坐标系下的-SINS integrated navigation and synthetic aperture radar program, geographic coordinates of the
Z3
- Z3惯导系统主要元部件,讲解了惯性系统元部件的知识-Z3 inertial navigation system is mainly yuan components, explained the components of the knowledge of inertial system yuan
xiejuandangel
- 惯性/无线电组合导航.采用无线电的原始输出信息与惯导组合-INS/VOR/DME
20091206_High_sensor
- 采用matlab/simulink仿真环境建立捷联惯导系统的垂向通道仿真模型,利用高度气压计进行增稳仿真,取得良好的高度通道稳定的效果。-The model of vertial channel was developed in matlab/simulink.By using the high sensor to upgrade the high stability.
platformalignment
- 平台惯导初始对准程序仿真-platform alignment
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
sins
- 惯导解算,采用二子样算法,补偿了旋转误差以及划桨误差。-INS Solution
pdf
- 全面介绍了惯导的基本知识,包括陀螺仪和加速度计,各种误差模型介绍。-introduction the inertial navigation good
SINS
- 捷联惯导Matlab仿真产生经昂及度纬度俯仰角等图形-Matlab simulation SINS
Strapdown
- 一、数据说明: 1:惯导系统为指北方位的捷连系统。初始经度为116.344695283度、纬度为39.975172度,高度h为30米。 初速度为v0=[0.000048637 0.000206947 0.007106781],飞行高度不变。 2:jlfw中为600秒的数据,陀螺仪和加速度计采样周期分别为为1/80秒和1/80秒。 3:初始姿态角为[0.120992605 0.010445947 91.637207](俯
INSjs
- 角增量 加速度增量 的捷联式惯导系统的 解算 程序-matlab SINS
CombinedNavigation
- 打击精度已经成为远程制导武器系统最重要的技术指标,提出了一种可以替代卫星导航的数据链导航系统,对 该系统的原理、实现、抗干扰、抗侦听进行了详细介绍,分析比较了该系统与惯导和卫星导航系统的误差。最后,得出了数据链 导航系统在武器装备精确制导中具有优势的结论。 -Precision has been the most important index to appraise a long-distance weapon under
jielianguandaojiesuan
- 捷联惯导系统解算程序包括MATLAB和C两个文件-SINS solver includes two files MATLAB and C