搜索资源列表
navi
- 该算法利用matlab实现指北方位捷联惯导解算过程-The algorithm uses matlab achieve refers northern bit SINS solver process
Cal_LeverArm
- 惯性导航系统结算过程中捷联惯导算法杆臂效应算法-Inertial navigation system in the the SINS algorithm rod arm effect algorithm
CNS
- 天文导航，弹道导弹SINS/CNS组合导航，轨迹发生器，卡尔曼滤波-Celestial navigation, ballistic missile SINS/CNS integrated navigation, trajectory generator, Kalman filtering
kfstatic
- 静基座下的SINS初始对准kalman滤波程序-The static base SINS initial alignment kalman filtering procedures
5
- 在GPS软件接收机和SINS辅助GPS跟踪技术的基础上,提出了一种SINS/GPS超紧致组合导航方案。该超紧致方案在GPS软件接收机的捕获环节中加入了基于相位估计的精细捕获算法,从而提高了频率捕获精度,省略了频率跟踪牵引过程 在信号跟踪环节中,利用SINS位置、速度信息与卫星参数,求取接收机与卫星之间的径向距离和径向距离率,为码环、载波环提供辅助,从而降低了载体动态变化对跟踪环的影响,提高了跟踪环的动态跟踪性能 同时,降低载波环噪声带宽
GPS_SINS
- 捷联惯导系统的导航算法，采用卡尔曼滤波对惯性信息和GPS信号进行融合，进行噪声处理-SINS navigation algorithm, Kalman filtering fusion of inertial information and GPS signal, noise processing
Direct
- dBasic principles of the strapdown inertial navigation system (SINS) using the outputs of strapdown gyros and accelerometers are explained, and the main equations are described. A mathematical model of SINS is establi
Direct_C_Noise
- Basic principles of the strapdown inertial navigation system (SINS) using the outputs of strapdown gyros and accelerometers are explained, and the main equations are described. A mathematical model of SINS is establish
GEN
- Basic principles of the strapdown inertial navigation system (SINS) using the outputs of strapdown gyros and accelerometers are explained, and the main equations are described. A mathematical model of SINS is establish
Indirect_Cancel
- Basic principles of the strapdown inertial navigation system (SINS) using the outputs of strapdown gyros and accelerometers are explained, and the main equations are described. A mathematical model of SINS is establish
denoise1
- 编写的小波去噪程序，主要用于光纤捷联惯导系统中的惯性器件输出噪声滤除，为后续导航解算提供基础-The wavelet denoising program written mainly used in fiber SINS the inertial device output noise filtering, to provide a basis for subsequent navigation solution
sins
- 捷连惯性导航,这是关于现在兴起的导航，采用仿真的形式-Jielian inertial navigation, which is now the rise of the navigation, the use of simulation in the form of
newSINS
- 关于惯导算法的一般程序，主要针对捷联惯导-Inertial navigation algorithm general procedures for SINS
DGP-SINS-Integrated-Pos
- 武汉大学的一篇关于INS/GPS组合导航的论文，非常经典，算法和实验结果都非常详细！用中国知网阅读器打开-Wuhan University, very classic article on the papers of the INS/GPS integrated navigation algorithms and experimental results are very detailed! Chinese HowNet reader
RungKutta
- GPS/捷联惯导组合导航中的龙格库塔法的解算，在matlab程序中使用-Runge-Kutta method for solving GPS/SINS integrated navigation, matlab program
INS-and-dead-reckoning-combination
- 捷联惯导与行位推算，构成组合导航系统，INS和航位推算组合-The SINS line reckoning that constitute the integrated navigation system, INS, and the combination of dead reckoning
Initial-alignment
- 捷联惯导初始对准程序，主惯导与子惯导初始对准-SINS initial alignment procedure, the main INS and sub-inertial alignment
my_sins
- 本程序实现SINS捷联解算，提供给惯性期间信息即可得到导航参数-The program SINS Jie associated solver, information provided to the inertia during navigation parameters can be obtained
longku_4
- 捷联惯导中用于计算四元数微分方程的四阶龙格库塔法matlab程序-SINS quaternion differential equations used to calculate the fourth-order Runge-Kutta method matlab program
strapdown
- matlab实现捷联惯性导航解算，四元数更新姿态矩阵。-SINS solver matlab