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Description: AVR自平衡车主程序，使用ENC-03陀螺仪和MMA7260作为传感器，内含卡尔曼滤波、PID-AVR owners of self-balancing process, the use of ENC-03 MMA7260 as gyroscopes and sensors, embedded Kalman filter, PID, etc.
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Size: 68079 |
Author: testsb |
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Description: 陀螺仪的驱动程序,用ATMEGA16编写,使用AD7715做AD采集,16BIT精度.-Gyroscopes driver, using ATmega16 prepared using AD7715 to do AD Acquisition, 16BIT accuracy.
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Size: 11264 |
Author: 邵亮 |
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Description: 一篇确定捷联惯导初始姿态的专利文章，通过设置监控陀螺对其他三个陀螺进行测漂-A determined attitude SINS initial patent articles, by setting the monitor to the other three gyroscopes to measure gyro drift
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Size: 627712 |
Author: liwei |
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Description: 陀螺仪材料，自动控制不可缺少的
对于其使用还需各位多多指点啊-Gyroscopes material, automatic control indispensable need for their use that a lot of pointing ah
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Size: 56320 |
Author: 离我 |
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Description: 几篇陀螺仪的有用的文章， 几篇陀螺仪的有用的文章-Gyroscopes several useful articles, a few useful gyroscope article
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Size: 795648 |
Author: 马红 |
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Description: 陀螺仪漂移特性的小波分析 陀螺仪漂移特性的小波分析-Gyroscope drift characteristics of the wavelet analysis of the characteristics of gyroscope drift gyroscopes drift wavelet analysis Wavelet analysis
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Size: 128000 |
Author: shmyg |
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Description: 一、数据说明：
1：惯导系统为指北方位的捷连系统。初始经度为116.344695283度、纬度为39.975172度,高度h为30米。
初速度为v0=[0.000048637 0.000206947 0.007106781]，飞行高度不变。
2：jlfw中为600秒的数据，陀螺仪和加速度计采样周期分别为为1/80秒和1/80秒。
3：初始姿态角为[0.120992605 0.010445947 91.637207]（俯仰，横滚，航向,单位为度）,
jlfw中保存的为比力信息f_INSc(单位m/s^2)、陀螺仪角速率信息wib_INSc(单位rad/s)，排列顺序为 一~三行分别为东、北、天向信息.
4: 航向角以逆时针为正。
5:地球椭球长半径re=6378245 地球自转角速度wie=7.292115147e-5 重力加速度g=g0*(1+gk1*c33^2)*(1-2*h/re)/sqrt(1-gk2*c33^2)；
g0=9.7803267714 gk1=0.00193185138639 gk2=0.00669437999013 c33=sin(lat纬度) -First, data on:
1: inertial navigation system that links the north bit of the Czech system. Initial longitude 116.344695283 degrees latitude 39.975172, height h is 30 meters.
Initial speed of v0 = [0.000048637 0.000206947 0.007106781], the same altitude.
2: jlfw for 600 seconds of data, gyroscopes and accelerometers were sampling period of 1/80 sec and 1/80 seconds.
3: Initial attitude angle [0.120992605 0.010445947 91.637207] (pitch, roll, heading, in units of degrees),
jlfw than the power saved information f_INSc (unit m/s ^ 2), angular rate gyro information wib_INSc (units of rad/s), in the order of 1 ~ three lines were east, north, days to the information.
4: The heading angle is positive counterclockwise.
5: Earth ellipsoid long radius re = 6378245 Earth s rotation angular velocity wie = 7.292115147e-5 acceleration due to gravity g = g0* (1+ gk1* c33 ^ 2)* (1-2* h/re)/sqrt (1-gk2* c33 ^ 2)
g0 = 9.7803267714 gk1 = 0.00193185138639 gk2 = 0.00669437999013
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Size: 401408 |
Author: 袁刚平 |
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Description: SYSTEM MODELLING AND PID CONTROL SYSTEM OF FOUR ROTOR HELICOPTER
Author:Amit Kumar,Saurav Kumar Singh,Dipti Ranjan Biswal
Abstract:Four Rotor helicopter as the name suggests has four rotors .The controls system for such a craft is complex, as it requires the synchronization of four individual motors. These motors must be closely controlled in order to account for variations between the motors (one motor slightly more powerful than the others will upset the equilibrium of the craft), and in order to effectively dampen external disturbance. We incorporated in our vehicle a closed loop PID control system which measured in-flight dynamics via three gyroscopes and one accelerometer.
-SYSTEM MODELLING AND PID CONTROL SYSTEM OF FOUR ROTOR HELICOPTER
Author:Amit Kumar,Saurav Kumar Singh,Dipti Ranjan Biswal
Abstract:Four Rotor helicopter as the name suggests has four rotors .The controls system for such a craft is complex, as it requires the synchronization of four individual motors. These motors must be closely controlled in order to account for variations between the motors (one motor slightly more powerful than the others will upset the equilibrium of the craft), and in order to effectively dampen external disturbance. We incorporated in our vehicle a closed loop PID control system which measured in-flight dynamics via three gyroscopes and one accelerometer.
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Size: 507904 |
Author: AMIT KUMAR |
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Description: This is an Adaptation of Stergios Roumeliotis 6 DOF Extended Kalman Filter. Includes classes for incorporating odometers, motors, GPS, accelerometers and gyroscopes. These classes were used to control the NASA Mars Rover-This is an Adaptation of Stergios Roumeliotis 6 DOF Extended Kalman Filter. Includes classes for incorporating odometers, motors, GPS, accelerometers and gyroscopes. These classes were used to control the NASA Mars Rover
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Size: 689152 |
Author: Kermit |
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Description: 卡尔曼滤波-很不错，使用于姿态校正，使用陀螺仪和加速度计来进行计算-Kalman filter- a very good posture correction used, the use of gyroscopes and accelerometers to calculate
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Size: 45056 |
Author: liu |
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Description: 这是我自己写的xsen的mti系统程序，从陀螺仪和加速度计中实时读取数据，并在地理坐标系中进行解算，最后积分得到速度和位置信息。可以用于手势识别或者精度要求不高的导航系统。如果要用于精确导航，则应该进一步进行修正。程序使用com4进行通信，波特率是115200，采样频率是50hz，这些参数都可以修改。-This is my own writing xsen the mti system program from the gyroscopes and accelerometers to read data in real time, and geographic coordinate system solver, the final points to get the speed and location information. Can be used for gesture recognition or less precision navigation system. If you want to for accurate navigation, it should be further amended. Program to communicate with com4, baud rate is 115200, the sampling frequency is 50hz, these parameters can be modified.
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Size: 1746944 |
Author: wuzhaojun |
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Description: AVR自平衡车主程序，使用ENC-03陀螺仪和MMA7260作为传感器，内含卡尔曼滤波、PID-AVR owners of self-balancing process, the use of ENC-03 MMA7260 as gyroscopes and sensors, embedded Kalman filter, PID, etc.
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Size: 67584 |
Author: kelvin |
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Description: 基于ATMEGA，用陀螺仪和加速度计实现自平衡小车设计-Based on ATMEGA, with gyroscopes and accelerometers to achieve self-balanced car design
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Size: 67584 |
Author: liao |
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Description: 用Matlab实现对惯性导航系统（陀螺仪和加速度计）的误差分析。-Matlab to inertial navigation system (gyroscopes and accelerometers) error analysis.
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Size: 1024 |
Author: 邱跳文 |
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Description: enc-03-mb陀螺仪的参考资料.e文的,很简单-Enc-03-mb gyroscopes references . E article, very simple
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Size: 504832 |
Author: rod |
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Description: 三轴转台的VB程序，通过陀螺仪控制三轴转台旋转，定角度。-Three-axis 转台 VB procedures , through gyroscopes control three-axis 转台 revolving , set point .
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Size: 24576 |
Author: 王伟峰 |
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Description: 滤波器，用于陀螺仪，加速度计，旋转角度的测量-Filtering code for gyroscopes, accelerometers, angle measurement
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Size: 319488 |
Author: Joseph |
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Description: 微型惯性测量组合包括微型陀螺仪和微型加速度计，是MEMS技术在惯性技术领域成功应用。与传统的惯性器件相比，MIMU在设计、材料和制造等方面都采用了全新的、革命性的工艺和方法，使其具有前所未见的小体积和重量、商业级的低价格、极高的可靠性和寿命。MIMU的这些特点使得惯性测量技术的应用从不计成本的军事领域扩展到市场广阔的民用、商用领域。-Micro inertial measurement units, including micro-gyroscopes and micro-accelerometers, MEMS technology is successfully applied in the field of inertial technology. Compared with the traditional inertial devices, MIMU in design, materials and manufacturing are adopting a new, revolutionary technology and methods, it has the unprecedented small size and weight, commercial-grade, low price high reliability and life. MIMU of these features make the inertial measurement technology from the military in the field regardless of cost to market a vast expansion of civil, commercial area.
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Size: 609280 |
Author: xiaoyi |
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Description: 旋转质量陀螺仪及其力学分析,介绍陀螺仪基本原理、特性，动力学特性-Spinning mass gyroscopes and their mechanical gyroscope basic principles, characteristics, dynamics
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Size: 611328 |
Author: 陈生 |
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Description: 使用labview控制陀螺仪的选择运动，实现三维仿真-Use labview control gyroscopes choice movement, to achieve three-dimensional simulation
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Size: 666624 |
Author: 刘维平 |
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