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技术资料 03 calgary PhD Development of a Low-Cost GPS-Based Attitude Determination System.pdf

资料->【E】光盘论文->【E1】斯坦福博士论文->03 calgary PhD Development of a Low-Cost GPS-Based Attitude Determination System.pdf
https://www.eeworm.com/dl/948896.html
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文章/文档 Particle Filtering for Sequential Spacecraft Attitude Estimation 卫星姿态估计的另外一种粒子滤波的介绍

Particle Filtering for Sequential Spacecraft Attitude Estimation 卫星姿态估计的另外一种粒子滤波的介绍
https://www.eeworm.com/dl/652/266984.html
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文章/文档 SPACECRAFT ATTITUDE DETERMINATION BY ADAPTIVE KALMAN FILTERING 介绍了一种基于自适应卡尔曼滤波的方法

SPACECRAFT ATTITUDE DETERMINATION BY ADAPTIVE KALMAN FILTERING 介绍了一种基于自适应卡尔曼滤波的方法
https://www.eeworm.com/dl/652/266960.html
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其他书籍 详细分析了姿态估值器与四元数估值器。ATTITUDE ESTIMATION OR QUARTERNION ESTIMATION

详细分析了姿态估值器与四元数估值器。ATTITUDE ESTIMATION OR QUARTERNION ESTIMATION
https://www.eeworm.com/dl/542/351321.html
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其他书籍 This paper deals with the issue of incorporating pseudolite measurements into an integrated Global P

This paper deals with the issue of incorporating pseudolite measurements into an integrated Global Positioning System/ Inertial Navigation System ~GPS/INS! positioning and attitude system with a view to improving signal availability, solution reliability, and accuracy in a localized area
https://www.eeworm.com/dl/542/324622.html
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电子书籍 This paper provides a rigorous comprehensive approach to the design of the principal software algor

This paper provides a rigorous comprehensive approach to the design of the principal software algorithmsutilized inmodern-day strapdown inertial navigationsystems: integration of angular rate into attitude, acceleration transformation/integration into velocity, and integration of velocity into posit ...
https://www.eeworm.com/dl/cadence/ebook/355777.html
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技术资料 基于MEMS的姿态测量系统

基于MEMS 的姿态测量系统A MEMS2Ba sed Attitude Reference System 载体的姿态测量是载体进行预计轨迹运动的基础。姿态测量有多种方式,其中采
https://www.eeworm.com/dl/914817.html
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数值算法/人工智能 This demonstration models a flight control for the longitudinal motion of a Grumman Aerospace F-14 T

This demonstration models a flight control for the longitudinal motion of a Grumman Aerospace F-14 Tomcat. First order linear approximations of the aircraft and actuator behavior are connected to an analog flight control design that uses the pilot s stick pitch command as the set point for the air ...
https://www.eeworm.com/dl/518/297040.html
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技术资料 一种车辆入库自动循迹停车系统的方案设计

汽车在现代社会生活中的普及程度越来越高,对停车环境和效率的要求也越来越高,先进的自动停车系统可以大大缩短停车的时间,提高停车位的利用率。本设计是一种在车库中应用的能够实现停车路线自动规划的系统,车辆进入车库就自动循迹并引导停车。该系统主要由环境数据采集子系统,中央控制子系统和车辆行驶姿态控制子系统组成。 ...
https://www.eeworm.com/dl/894659.html
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技术资料 基于STC单片机的自平衡小车设计

本文提出了一种两轮自平衡小车的设计方案,采用集成了3轴MEMS陀螺仪与3轴加速度MPU6050构成小车姿态检测装置,完成陀螺仪数据与加速度计数据的数据融合。系统选用STC15系列1T8051单片机IAP15W4K63S4为控制核心,完成传感器信号的处理及车身平衡控制。系统各个模块能够正常并协调工作,小车可在无人干预条件下实现自主平衡。In t ...
https://www.eeworm.com/dl/897727.html
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