ATTITUDE
共 23 篇文章
ATTITUDE 相关的电子技术资料，包括技术文档、应用笔记、电路设计、代码示例等，共 23 篇文章，持续更新中。
96 calgary PhD Development of a Real-time Attitude System Using a Quaternion Parameterization and No
资料->【E】光盘论文->【E1】斯坦福博士论文->96 calgary PhD Development of a Real-time Attitude System Using a Quaternion Parameterization and Non-Dedicated GPS Receivers.pdf
01 Auburn PhD Real-time attitude determination using the global positioning system.pdf
资料->【E】光盘论文->【E1】斯坦福博士论文->01 Auburn PhD Real-time attitude determination using the global positioning system.pdf
95 calgary PhD Development of a GPS Multi-Antenna System for Attitude Determination.pdf
资料->【E】光盘论文->【E1】斯坦福博士论文->95 calgary PhD Development of a GPS Multi-Antenna System for Attitude Determination.pdf
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
92 Stanford PhD Attitude determination using GPS ClarkCohenThesis92.pdf
资料->【E】光盘论文->【E1】斯坦福博士论文->92 Stanford PhD Attitude determination using GPS ClarkCohenThesis92.pdf
基于MEMS的姿态测量系统
<P>基于MEMS 的姿态测量系统A MEMS2Ba sed Attitude Reference System</P>
<P>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
Attitude Controller Design on Variable Rolling Velocity Aerocraft Based on ATmega16
Owing to the effect of crosswind, initial disturbance and the deviation of engine parameters.etc in
翻转校园下单片机实验教学方法改进
<p>MCS51单片机的实验有8个,主要是端口的操作.在proteus仿真实验,并利用MCS51单片机试验箱验证.学生做好实验后,利用翻转校园的测试功能,测试学生对实验课的掌握程度,同时利用翻转校园的评学功能,对学生的实验结果进行评价,最后利用翻转校园的讨论功能,讨论这节课学到的内容.这样做,加深了学生的记忆,对学生的实验结果评价后,学生实验课更加认真,课堂讨论对一些疑难问题进行讨论后,加深了学生
基于AVR单片机的四旋翼飞行器的设计
<p>四旋翼飞行器具有机械结构简单、成本低、事故率低、重量轻等优点,因此应用前景广泛。文章以Arduino Mega2560单片机为核心控制器设计一架小型四旋翼飞行器。首先,通过主控制器、惯性测量单元、遥控通信模块、电源与驱动模块完成系统的硬件结构设计。其次,采用卡尔曼滤波来消除干扰,以及利用四元数算法解算出飞行姿态角控制电机的转速,并通过双闭环串级PID控制来调节飞行器的平衡性。最后采用C语言编
基于STC单片机的自平衡小车设计
<p>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。</p><p>In this paper, a desig
一种车辆入库自动循迹停车系统的方案设计
<p>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。其中车辆行驶姿态控制子系统主要涵盖路线生成与自动循迹等;环境数据收集子系统包括信号接收和传
01 California PhD Tightly integrated attitude determination methods for low-cost inertial navigation
资料->【E】光盘论文->【E1】斯坦福博士论文->01 California PhD Tightly integrated attitude determination methods for low-cost inertial navigation-Two-antenna GPS and GPS-magnetometer.pdf
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 at
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
Spacecraft Attitude Dynamics and Control 航天器姿态控制的课件
Spacecraft Attitude Dynamics and Control 航天器姿态控制的课件，十分难得；内容通俗易懂；十分完整；是从事航天研究的必须知识
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
digit book about attitude on mobile
digit book about attitude on mobile
satellite attitude determination
satellite attitude determination
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
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