搜索资源列表
UKF-master
- 捷联惯导系统UKF算法的传递对准方面的研究程序，非常实用-The strapdown inertial navigation system transfer alignment of UKF algorithm research program, very practical
Dynamic-Identification
- The article considers different approaches to justify the possibility of using actual navigation information obtained public transportation buses in order to identify a new energy criterion, i.e. speed vector of “floating” cars. Under certain circu
Dynamic-Identification
- The article considers different approaches to justify the possibility of using actual navigation information obtained public transportation buses in order to identify a new energy criterion, i.e. speed vector of “floating” cars. Under certain circu
sanwei2
- 比例导引法跟踪做简单正弦机动目标的制导模型-Proportional navigation guidance tracks do simple sinusoidal model maneuvering target
zld2attitude
- 捷联惯导系统姿态解算，从IMU读入数据，输出数据与INS进行比对-Attitude Algorithm in Strap-down Inertial Navigation System
LI
- ins gps 组合导航程序，包括估计和卡尔曼滤波。-Ins gps integrated navigation program, including estimation and Kalman filtering
SINS
- 使用C语言写的捷联惯导解算程序，四子样旋转矢量-Using C language to write the strapdown inertial navigation program, four sample rotation vector
GPS_INS111
- 使用MATLAB写的惯性卫星组合导航卡尔曼滤波器程序-Using MATLAB to write inertial satellite combination navigation Kalman filter program
guandaofangzhen
- 实现了基于惯性导航定位的matlab仿真，并结合无线定位数据进行融合输出(The MATLAB simulation based on inertial navigation and positioning is realized, and the output is fused with the wireless positioning data)
psins151009
- 惯性导航分析工具箱 matlab工具箱 组合导航 卡尔曼滤波(this toolbox can be used to analysis the navigation system and assist to do some simulation on navigation system.)
SUAS_Code
- estimation of states of imu
psins程序
- 惯导算法，惯性导航工具箱最新版，卡尔曼滤波(Inertial navigation algorithm, the latest version of the navigation toolbox)
MATLAB
- 用比力导引法，计算某条件下算惯性器件在飞行期间内的敏感测量输出数值、导航输出数值(By using the method of specific force guidance, the sensitive measurement output value and the navigation output value of the inertial device during the flight are calculated.)
基于图像处理与北斗导航的目标区域定位方法研究
- 飞机上带有北斗导航或者GPS等定位装置，能够实时确定飞机的空间位置，获得其高度，经纬度等信息；飞机上载有光电吊舱，能够从高空拍摄图像或视频，并且能够通过其自带的传感器实时获得光电吊舱自身的倾斜角度、视场角度等信息；结合飞机所处的空间位置，光电吊舱的倾斜角度、视场角度以及地理信息系统就可以计算出光电吊舱所看到的区域所在的地理位置，并在地理信息系统中显示出其区域；若对图像中的某一局部区域感兴趣，需要确定其地理位置，则可通过鼠标点击这一区域，程序就能主动地计算出目标地点的地域坐标，并映射到地理信息系统
dubins
- dubins路径规划与相应的比例导引，模型采用过载控制(Dubins path and proportional navigation)
惯性导航
- 高精度惯性导航，解算程序，实验轨迹生成，来进行对比(High precision inertial navigation, solution program, experimental trajectory generation, for comparison)