Description: 用于惯性导航的初始对准，采用北东地坐标系，10个状态量-for use in inertial navigation initial alignment using the North East to coordinate system, 10 state variables Platform: |
Size: 2365 |
Author:谢鹏 |
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Description: 用于惯性导航的初始对准，采用北东地坐标系，10个状态量-for use in inertial navigation initial alignment using the North East to coordinate system, 10 state variables Platform: |
Size: 2048 |
Author:谢鹏 |
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Description: 这是本人编写的一个接联惯性导航系统解析粗对准的仿真程序，其中分别采用了传统和改进的解析对准算法。-This is the one I prepared received Inertial Navigation System Analysis rough at the simulation program, which were used to the traditional and improved analytical alignment algorithm. Platform: |
Size: 2048 |
Author:吉庆昌 |
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Description: 这是一个本人编写的一个接联惯性导航系统解析粗对准程序可观测性分析的一个程序。-This is the one I prepared received an Inertial Navigation System Analysis rough alignment procedures observability analysis of a trip sequence. Platform: |
Size: 1024 |
Author:吉庆昌 |
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Description: 这是本人用SIMLINK辨析的一个用经典控制理论方法实现的接联惯性导航系统精对准的方法程序。-using SIMLINK Analysis with the use of a classical control theory method of access inertial navigation systems EC precision alignment methods and procedures. Platform: |
Size: 6144 |
Author:吉庆昌 |
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Description: 工学博士学位论文 目前，扩展卡尔曼滤波是研究初始对准和惯性/GPS组合导航问题的一个主要手段。 但初始对准和惯性/GPS组合导航问题本质上是非线性的，对-Engineering PhD thesis Currently, EKF is the initial alignment study and inertial/GPS navigation of a major means. However, initial alignment and inertial/GPS navigation on the nature of the problem is nonlinear, Platform: |
Size: 7168 |
Author:lv |
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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. Platform: |
Size: 8600576 |
Author:王琴 |
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Description: 在捷联式惯性导航系统中，惯性敏感器直接固联在载体上，惯性敏感器的工作条件和环境与单独测试惯性敏感器时有较大的差别。并且当惯性敏感器安装到惯性组件上以后，还存在各种安装误差，因此对惯性敏感器单独测试的结果并不能反映惯性敏感器在系统中实际的
性能品质。为了保证系统的技术性能，现代捷联惯性导航系统均采取了较为全面的误差补偿
措施。捷联惯性导航系统误差补偿的前提则是对惯性组件进行精确的误差标定。
-In strapdown inertial navigation systems, inertial sensors is in direct solid carriers, inertial sensors, working conditions and environment with a separate test inertial sensors greater difference. And when the inertial sensor installed after inertial components, there is a variety of installation errors of inertial sensor test results alone do not reflect the inertial sensor in the system, the actual quality performance. In order to ensure the system Platform: |
Size: 248832 |
Author:申亮 |
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Description: Because of the poor observability of Inertial Navigation System on stationary base, the estimation
error of the azimuth will converge very slowly in initial alignment by means of Kalmari filtering, and making the
time initial alignment is longer. In this paper, a fast estimation method of the azimuth error is creatively proposed
for the initial alignment of INS on stationary base. On the basis of the the fast convergence of the leveling error,
the azimuth error can be directly calculated. By means of this fast initial alignment method, the time of initial
alignment is reduced greatly. The computer simulation results illustrate the efficiency of the method. Platform: |
Size: 188416 |
Author:huzhou |
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Description: 自己编写的鲁棒滤波算法的应用，应用于惯性导航系统初始对准中，静止基座-I have written the application of robust filtering algorithm used in inertial navigation system in the initial alignment, static base Platform: |
Size: 10240 |
Author:gaoxu |
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Description: 自己编写的kalman滤波算法的应用，应用于惯性导航系统初始对准中，运动基座-I have written the application of kalman filtering algorithm used in inertial navigation system in the initial alignment, sports base Platform: |
Size: 30720 |
Author:gaoxu |
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Description: 本书为东南大学出版社的万德钧, 房建成等《惯性导航系统初始对准》 采用超星可以阅读-This book is Southeast University Publishing House-Jun Wan, Fang Jiancheng, etc., " Inertial Navigation System Alignment" can be read by Superstar Platform: |
Size: 2970624 |
Author:kent |
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Description: 关于惯性导航技术中的一个小的利用四元数算法求解姿态的程序，简单实用-Inertial navigation technology on a small initial alignment procedures to achieve a calculated INS s initial posture Platform: |
Size: 3072 |
Author:王珂 |
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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 Platform: |
Size: 654336 |
Author:caijianan |
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Description: 基于惯性系粗对准，实测可用,自己的毕业论文的结果-Based on the inertia system rough alignment, measured available Platform: |
Size: 873472 |
Author:导航疯狂研究者 |
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