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Description: 捷联惯导初始误差及仿真,是个不错的文章啊-SINS initial error and simulation is a good article ah
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Author: greatshao |
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Description: 硕士学位论文捷联惯性系统初始对准研究
惯导系统的初始对准是影响系统使用性能的关键技术之一，对准的精度与速度直接关系到惯性统的精度与启动特性。对卡尔曼滤波及其在初始对准中的应用进行了研究。首先介绍了卡尔曼滤波理论的应用背景，然后推导了离散卡尔曼滤波方程，并对连续系统的状态方程进行离散化提出了适用于舰载捷联惯性系统的动基座对准的2通道10个状态变量和2通道12个状态变量的系统动态模型，并建了相应的速度匹配和位置匹配量测模型。
-master's degree thesis SINS initial alignment study INS initial alignment is affecting system performance one of the key technologies, the alignment precision and speed is directly related to the precision inertial reunification with the startup characteristics. The Kalman filter and the initial alignment of the study. First introduced the theory of Kalman filtering background, and then reasoned a discrete Kalman filter equations, also for the state of discrete equations apply to the carrier SINS System Moving Base Alignment of two channels 10 state variables and two 12-channel system state variables dynamic model and built a corresponding speed matching and position matching measurement model.
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Size: 8600889 |
Author: 王琴 |
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Description: 初始对准的c算法源码,实现捷联惯导的静基座初始对准-c initial alignment algorithm source code, achieving SINS the static base initial alignment
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Size: 358400 |
Author: zhengjun |
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Description: 捷联惯导初始误差及仿真,是个不错的文章啊-SINS initial error and simulation is a good article ah
Platform: |
Size: 4550656 |
Author: greatshao |
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Description: 硕士学位论文捷联惯性系统初始对准研究
惯导系统的初始对准是影响系统使用性能的关键技术之一，对准的精度与速度直接关系到惯性统的精度与启动特性。对卡尔曼滤波及其在初始对准中的应用进行了研究。首先介绍了卡尔曼滤波理论的应用背景，然后推导了离散卡尔曼滤波方程，并对连续系统的状态方程进行离散化提出了适用于舰载捷联惯性系统的动基座对准的2通道10个状态变量和2通道12个状态变量的系统动态模型，并建了相应的速度匹配和位置匹配量测模型。
-master's degree thesis SINS initial alignment study INS initial alignment is affecting system performance one of the key technologies, the alignment precision and speed is directly related to the precision inertial reunification with the startup characteristics. The Kalman filter and the initial alignment of the study. First introduced the theory of Kalman filtering background, and then reasoned a discrete Kalman filter equations, also for the state of discrete equations apply to the carrier SINS System Moving Base Alignment of two channels 10 state variables and two 12-channel system state variables dynamic model and built a corresponding speed matching and position matching measurement model.
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Size: 8600576 |
Author: 王琴 |
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Description: 该原代码包括捷联惯导姿态程序,位置程序以及初始对准程序,实用性强,便于学习.-The original code, including procedures SINS posture, location, procedures and initial alignment procedures, practical, easy to learn.
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Size: 5120 |
Author: 119911 |
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Description: 介绍了捷联惯性导航初始对准的几种方法，包括经典对准和卡尔曼滤波对准，有利于初学者学习。-Introduction of SINS initial alignment of several methods, including the classic Kalman filter alignment and alignment will help beginners to learn.
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Size: 2970624 |
Author: tlj |
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Description: 捷联惯导初始对准Kalman滤波程序，matlab编写-SINS initial alignment Kalman filter procedure, matlab prepared
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Size: 2048 |
Author: 钱伟 |
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Description: matlab应用于捷联惯导系统初始对准滤波技术程序-matlab applies SINS initial alignment procedures Filtering Technique
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Size: 11264 |
Author: 孙柏虹 |
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Description: 本程序是关于四元数法捷联惯导解算算法的matlab程序组合包，其中包括滤波初始对准仿真，罗经法初始对准仿真，捷联惯导解算仿真，组合卡尔曼滤波等演示程序及其必需的参数矩阵转换程序，程序算法皆是本人通过大量阅读捷联惯导经典论文书籍编写的，经过调试已经通过，所得圆锥误差，划桨误差与秦永元所编惯性导航一书相符，可靠性较高。适合惯导学习者参考改进使用
-This procedure is the law about quaternion SINS algorithm matlab solver combination package procedures, including filtering at the initial simulation, the initial alignment Gyrocompass law simulation, SINS Solution Demo simulation procedures, portfolio Kalman filter and the necessary presentation matrix conversion process parameters, the program algorithm are a large number of read I SINS classic books written thesis, after debugging has been passed from the error cone, paddle QIN Yong-yuan of the error and inertial navigation for one book in line with higher reliability. Inertial reference suitable to improve the use of learners
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Size: 20480 |
Author: lijipeng |
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Description: 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
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Size: 152576 |
Author: pei fu-jun |
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Description: EKF在捷联惯性导航系统初始对准中的应用？在方位角为大失准角的情况下，如何进行初始对准-EKF in SINS Initial Alignment? In the azimuth misalignment angle for the big cases, how to initial alignment
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Size: 4096 |
Author: yangjunwei |
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Description: 捷联惯导初始对准的程序 matlab写的 包括动基座和静基座对准。-Initial Alignment of SINS program written in matlab, including dynamic and static alignment.
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Size: 160768 |
Author: zhou |
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Description: 本文针对捷联惯导系统(SINS)初始对准问题,提出了一种无需经历传统的粗对准阶段而利用单天线GPS辅助直接进行动基座精确初始对准的新方法
-In this paper, SINS (SINS) initial alignment problem, we propose a coarse alignment without experiencing the traditional stages of a single-antenna GPS-assisted direct precise moving base initial alignment of the new method
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Size: 107520 |
Author: liuhaipeng |
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Description: 本文提出了一种基于转动基座的快速估计平台失准角的初始对准方法，研究了扩展观测量的Kalman滤波算法，指出转动基座初始对准的可观测度优于传统最优二位置对准。-This paper presents a quick estimate based on rotating base platform misalignment angle of the initial alignment method to study the extended observations of the Kalman filtering algorithm, that the initial alignment of the rotating base considerably superior to the traditional measure of the optimal two position alignment.
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Size: 260096 |
Author: liuhaipeng |
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Description: 本文在运载体运动情况下，提出了一种适用于捷联惯导系初始对准的新算法，该算法以
惯性空间为参考基准，将初始对准姿态矩阵的实现分解为三部分-This movement of the transporter, the paper presents a system for SINS Initial Alignment of the new algorithm to inertial space as the reference point, the realization of initial alignment attitude matrix is decomposed into three parts
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Size: 329728 |
Author: liuhaipeng |
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Description: 捷联惯导系统初始对准几种不同滤波方法对比matlab程序-SINS initial alignment of several different filtering matlab program
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Size: 656384 |
Author: 白开水 |
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Description: 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
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Size: 654336 |
Author: caijianan |
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Description: 双历元GNSS辅助SINS动态初始对准方法，获得初始时刻的位置、速度、姿态等的信息。含有初始对准程序以及测试程序，四元数计算程序-Dual Dynamic epoch GNSS assistance SINS initial alignment method to obtain the initial time position, velocity, attitude and other information. Containing the initial alignment procedures and testing procedures, quaternion calculation program
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Size: 10240 |
Author: yaboyuan |
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Description: 捷联惯导初始对准的C源码 -SINS initial alignment of the C source, including
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Size: 196608 |
Author: zhchwl |
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