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- 有关自动控制方面的惯性环节响应，matlab仿真程序-control of the inertial response link, Matlab simulation program
INSgongjuxiang.rar
- 一个惯导的工具箱，很实用，学习惯导的可以应用此工具箱来实现自己程序的编写,An inertial navigation toolbox, it is useful to learn INS can be applied to the toolbox to achieve their own procedures for the preparation of
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]（俯仰，横滚，航向,单位为度）, jlfw中保存的为比力信
GPSandINS
- 在MATLAB环境下，使用GPS与惯性导航技术相结合的联合导航卡尔曼滤波算法-In the MATLAB environment, the use of GPS and inertial navigation technology joint navigation Kalman filter algorithm
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
INS_GPS_integrated_navigation_system
- 通过卡尔曼滤波并采用开环控制方式实现惯性导航和GPS的数据融合-Through the Kalman filter and use the open-loop control method to achieve inertial navigation and GPS, data fusion
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
global-positioning-systems-inertial-navigation-an
- This book constitutes an excellent source for understanding the basic operation of the Global Positioning Systems (GPS). It also allows the reader to take the first steps towards understanding how the Kalman Filter is implemented in the estimation of
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
GPS_INS_KF
- MatLab Files for GLOBAL POSITIONING SYSTEMS, INERTIAL NAVIGATION, AND INTEGRATION
EKF
- Extended Kalman Filter synthesis for integrated global positioning/inertial navigation systems
inertial
- 用Matlab实现对惯性导航系统（陀螺仪和加速度计）的误差分析。-Matlab to inertial navigation system (gyroscopes and accelerometers) error analysis.
Aircraft-inertial-navigation-control-system-desig
- Aircraft inertial navigation control system design and simulation platform implementations
Paul_G.Savage
- GNSS接收机惯性导航处理算法技术文档,用于提高导航接收机性能，在高动态环境下具有良好的稳健性-technique paper for GNSS receiver inertial navigation algorithm
Strapdown-inertial-navigation
- 一个简单的捷联姿态解算算法 GPS-INS惯导算法-A simple strapdown attitude solver algorithm GPS-INS inertial navigation algorithm
Inertial-sensor-development
- 随着GPS性能的不断完善，应用越来越广泛，但GPS系统易受到外界环境影响，而传统的惯导系统也具有误差随时间积累的缺陷，因此GPS/INS组合方式因其互补性强已经成为实现导航的重要方式。这种组合方式能够确保在采用较廉价的惯性设备的情况下，也能获得较好的导航效果。-With the constant improvement of the GPS performance, more and more widely, but the GPS system vulnerable to external e
inertial-navition
- 基本的惯性导航解算过程以及摇摆条件下的惯性导航程序-Inertial navigation program under the basic inertial navigation solution process and the swing conditions
two-sample-inertial-algorithm
- 基于MATLAB的双子样惯导解算算法实现，可以直接调用-A mfile based on the MATLAB of the two- type inertial navigation algorithm algorithm to achieve, which can be called directly.
inertial-navigation-algorithm
- inertial navigation algorithm matlab program, a routine