搜索资源列表
sins
- 捷联与平台惯导静基座初始对准程序,C语言编写,很好的例程-Strapdown inertial navigation static base and the platform initial alignment process, C language, a good routine
jielian
- 捷联惯导仿真程序。针对于一般飞行器应用的捷联惯导系统,选择以地理坐标系为导航坐标系,根据指北方位系统的导航原理进行力学编排及数值仿真;制导系统针对于一般的弹道导弹,设计标准弹道,比较摄动制导与显式制导的优劣性,选择灵活性较好、适应性较强的显式制导,以待增速度为关机函数,控制关机,使之命中目标。-sins simulation
INSandGPS
- 捷联惯导GPS组合导航Kalman滤波器-SINS GPS Navigation Kalman Filter
Strapdown
- 《Strapdown inertial navigation technology》全面系统地介绍了捷联惯导的基本原理与计算。-Strapdown inertial navigation technology, a comprehensive and systematic introduction to the basic principles of strapdown inertial navigation system and calculation.
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
Fast-Initial-Alignment
- 直接利用两水平失准角快速收敛的估计结果对传统多位里对准中方位失准角的估计,提高了捷联惯导系统静基座对准的精度和速度。-Two level losing accuracy angle rapid convergence directly the estimate result to traditional many to the position losing accuracy angle estimate, thus increased the precision which and the s
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)
20697951another
- 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 the strapdown inertial navigation of another kind of calculating method, including calculating the position, velocity and attitude)
jielian
- 捷联惯导的程序,算法比较简单,运行速度比较快(Strapdown inertial navigation program, the algorithm is simple, fast operatio)
KF_SINS
- 本程序为捷联惯导系统静基座对准卡尔曼滤波程序,观测量为水平速度误差,程序经本人验证正确无误。(This program is a static mount of strapdown inertial navigation system (SINS). It is a Calman filtering program, and the observation is horizontal velocity error. The program is proved correct by myself.
PSINS-CPP
- 捷联惯导算法C++程序,严龚敏老师PINS工具箱C++版本(Strapdown inertial navigation algorithm C++ program, Yan Gongmin teacher PINS toolbox C++ version)
捷联惯导角速度匹配传递对准方法研究
- 用二阶马尔可夫对舰体变形进行了建模,并对角速度匹配传递对准方法进行了研究。计算机仿真验证了舰体变形模型的可行性,角速度匹配传递对准方案可以有效、快速地为潜器提供高精度的导航姿态基准。(The ship body deformation is modeled by two order Markov model, and the method of diagonal velocity matching transfer alignment is studied. The feasibility of
捷联惯导及其组合导航研究
- 本文对捷联惯导系统(sINS)及其与全球定位系统(GPS)的组合导航系统进行 了研究。首先对实现S取S的初始对准及姿态矩阵计算等关键技术进行了系统研究。 在仿真的基础上进行了实际捷联惯导系统的系统研制,针对陀螺漂移补偿等关键算法 开展深入研究,实验结果表明经过补偿解算后,整个捷联惯导系统导航参数的解算精 度大大提高。在实现SINS的基础土,研究了SINS与GPS(The strapdown inertial navigation system (sINS) and global posi
SINS
- 捷联惯导算法、四元数算法姿态解算、误差补偿及仿真分析,matlab仿真程序(Attitude calculation of strapdown inertial navigation system algorithm based on Matlab)
psins简化版150914
- 严恭敏捷联惯导算法工具箱,可使用,对研究SINS有所帮助(Yan Gong agile inertial navigation algorithm toolbox, available and helpful to the study of SINS)
psins160731
- 捷联惯导仿真装置设计例程包括四元函数分析等主函数和子函数(Four element function method for the design of strapdown inertial navigation simulator)
csdz
- 捷联惯导初始对准MATLAB仿真文件,应用卡尔曼滤波(SINS initial alignment MATLAB simulation files, using Calman filtering)
matlab源程序及说明
- 关于捷联惯导与多普勒计程仪组合导航的算法程序,比较基础。方便初学者尝试(The algorithm program of SINS and Doppler Log integrated navigation is comparatively basic. Easy for beginners to try)
捷联惯导
- 以系统经度为横轴,纬度为纵轴(单位均要转换为:度)作出系统位置曲线图; (2) 作出系统东向速度和北向速度随时间变化曲线图(速度单位:m/s,时间单位:s); (3) 分别作出系统姿态角随时间变化曲线图(俯仰,横滚,航向,单位转换为:度,时间单位:s)(Taking the longitude of the system as the horizontal axis and the latitude as the longitudinal axis (the unit shoul
exp1
- 捷联惯导系统放置在室内测试台上做静态测试,测试时间4500s。 1)取前180数据做粗对准(解析对准法); 2)取第181s~900s数据做精对准(Kalman滤波法); 3)从第901s开始做纯惯导解算; 4)用国军标的导航系统位置精度评价方法评估系统定位精度(分别计算CEP50 和 CEP95 下的定位精度)。(The strapdown inertial navigation system was placed on the indoor test bench for stati