搜索资源列表
SIM_IMU
- 惯性导航算法,实现陀螺仪的仿真,用于陀螺选型-inertial navigation algorithm, and the simulation gyroscope for gyro Selection
Mti
- 惯性测量组件Mti进行数据采集，利用陀螺和加速度计数据进行捷联姿态角解算，采用四元数更新算法，解算周期可调。
trajection
- 用Matlab编写的轨迹发生器，输入初始的位置速度，姿态角，姿态变化等信息，模拟得到陀螺仪输出和加速度计的输出-Written with the Matlab path generator, enter the initial position, velocity, attitude, attitude changes and other information, the simulated gyro output and the output of the accelerometer
sins
- 该程序包括了飞行器轨迹计算、陀螺和加速度计的采样输入、以及由四元素解算出的飞行器姿态、位置、速度-The program includes the aircraft trajectory calculation, the sampling gyro and accelerometer input, and the solution calculated by the four elements of aircraft attitude, position, velocity
imu_ahrs
- 基于IMU(三轴角速率、三轴加速计和三轴磁场)的方位姿态解算系统(ahrs)，基于C语言开发，VC 6.0编译器，可方便的移植到其他环境。-Based on the IMU (three-axis angular rate, three-axis accelerometer and three-axis magnetic field) to locate gesture Solution System (ahrs), based on C language development, VC 6.0
Simp_Unscented
- 抖动的存在，陀螺输出脉冲数在正负200之间跳动；其频谱表现为在抖动频率处的一个能量非常高（14000）的谱线；500～1000赫兹之间也有40左右的能量，表明陀螺输出存在一定的高频噪-The existence of jitter, gyro output pulses beating in between plus or minus 200 the performance of its spectrum in the frequency jitter of a very high energ
MicrostoneGyroSensor
- 高速陀螺数据手册 奥巴马已经限制出口中国的芯片 开发导弹需要使用到的技术-High-speed gyro data sheet limits of Obama' s chip exports to China need to develop missile technology
Navigation_integration_algorithm
- 最近在弄陀螺稳定，得到这篇很经典的资料，江南航天集团的。捷联式惯性导航积分算法。很稀罕的。-Get gyro stabilized recently received information of this classic, Jiangnan Aerospace Group. Strapdown inertial navigation integration algorithm. Very rare for.
Attitude_Kalman_gom
- 卡尔曼滤波器，具体组合为轨道罗盘+磁强计+速率陀螺，具体物理含义请见附件中的注释，航天人可以一目了然-Kalman filter, the specific combination of orbital compass+ magnetometer+ rate gyro, the specific physical meaning, please see attached comments in the space one can at a glance
Kalman_sgm
- 卡尔曼滤波器，敏感器组合形式为数字太阳敏感器+磁强计+速率陀螺，具体的参数物理含义请见文件中的注释，航天人依旧一目了然-Kalman filter sensor combinations for the digital sun sensor+ magnetometer+ rate gyroscope, specifically the physical meaning of parameters see comments in the file, astronauts still at a gl
C_newtyle
- 航天常用姿态确定敏感器组合，太阳敏感器+速率陀螺+轨道罗盘，具体数据含义请参考章仁为的<《卫星姿态控制》>-Spacecraft attitude determination sensors commonly used in combination, sun sensor+ rate gyro compass+ tracks, the meaning of specific data please refer to Chapter Ren' s < " Satell
GY_80_9axi_BMP085
- 陀螺及加速度计和压力计组合成的方位解算软件，51单片机实现的解算。方位较为准确。-The azimuth gyroscope and accelerometer and manometer combined into solver software, to 51 MCU solver. The orientation is more accurate.
STIM202
- 该文档描述了STIM202三轴陀螺仪的特性特征，在角度测量方面比较精确-This document describes the STIM202 axis gyroscope characteristic feature accurate angle measurement
kalman_wwh
- 实现GPS/INS组合导航解算位置、速度、航向等参数。输入数据：东向位置、北向位置、航向角（度）、gps速度、陀螺仪角速度、里程计脉冲数-Implement integrated GPS/INS navigation solution position, speed, course and other parameters. Input data: east position, north position, heading angle (degrees), gps speed, angular
IMU
- 采用加速度计和陀螺仪互补滤波获得载体三维姿态。-Using accelerometer and gyroscope carrier complementary filter to get 3 d pose.
duoziyang
- 由飞机陀螺仪所给出的数据，分别通过单子样，双子样，四子样方法进行飞行姿态的解算-Data the aircraft gyroscope given, respectively, through the list like, like Gemini, four sub-sample method Attitude solver
L3G4200D
- 陀螺仪的具体工作过程，指的是在无人机行业的应用-Detailed work process of gyroscope, refers to the application of unmanned aerial vehicle (uav) industry
Attitude-Algorithm
- 两种基于互补滤波的姿态算法，对陀螺仪和加速度计进行数据融合，解算姿态。一种使用了梯度下降算法，另一种使用反馈修正和李雅普诺夫分析。-Two algorithms for attitude estimate based on complementary filtering. Data form Gyroscope and Accelerometer are fused. One is based on gradient descent algorithm while the other is ba
psd-glpu
- matlab功率谱图，可以通过它对陀螺仪或加速度进行噪声误差分析，已经取得很好效果，请放心使用-matlab power spectrum, it can be a gyroscope or an acceleration noise error analysis, we have achieved very good results, ease of use
附有陀螺边的导线网平差软件
- 实现附有陀螺边的导线网平差，减轻外内业工作量，提高工作效率(Achieve with the gyro side of the wire network adjustment, reduce the workload of the outside home, improve work efficiency)