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Description: 基于C8051F530的SPI应用程序,读取传感器ADIS16355的信号
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Size: 6741 |
Author: yxh032571@126.com |
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Description: 基于S3C2440 ARM CPU, 通过IO接口模拟SPI接口,读取ADSI16355陀螺仪数据源码
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Size: 2010739 |
Author: guohuicao@126.com |
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Description: lpc2148 communicate with IMU ADIS16350 through SPI
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Size: 53248 |
Author: hbaocr |
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Description: ADIS16355的测试程序,并通过串口输出。-ADIS16355 testing procedures, and the output through the serial port.
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Size: 2048 |
Author: wang |
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Description: 利用单片机的标准SPI接口,读取姿态传感器ADIS16355的信号-The use of a standard SPI interface to MCU, reading attitude sensor signals ADIS16355
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Size: 19456 |
Author: 秦硕 |
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Description: 在keil c开发环境下,采用C语言编写的对ADIS16355惯性测量单元的测试程序,希望能有所帮助-In keil c development environment, written using C language on the ADIS16355 inertial measurement unit testing procedures, hoping to help
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Size: 67584 |
Author: 毛江飞 |
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Description: 用C8051F 读取ADIS16355中的数据-he use of a standard SPI interface to MCU, reading attitude sensor signals ADIS16355
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Size: 7168 |
Author: 医者 |
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Description: AD公司ADIS16355 C语言驱动程序,包含控制指令,数据读取指令,可移植性好,可直接使用,已有使用产品-AD ADIS16355 C language driver for the company, including control instructions, data read instructions, portability, and can be used directly, has been using the product
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Size: 2048 |
Author: wenjiefeng |
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Description: The open source project DSP_INS is an inertial navigation system on the TI DSP
platform TMS320F28335 with MEMS inertial sensors and commercial GPS module. Inertial
sensors are actually used only for estimating attitude, heading and velocity.
Position information totally comes from GPS (see Q2 in FAQ part). Currently the
MEMS IMU (Inertial Measurement Unit) ADIS16355 and GPS module u-blox LEA-5H
are supported. DSP_INS also reads magnetic field data from HONEYWELL HMC1051/1052.
You can also use the latest IMU module ADIS16405, which also contains magnetic field
sensors.
There is a 10-order extended Kalman filter in DSP_INS, which takes angular velocity,
acceleration, magnetic field, and GPS velocity as inputs. It provides outputs
including angular velocity, acceleration, attitude, heading, velocity, and position
(from GPS) every 10 milliseconds. DSP_INS is proved to be effective and reliable in
several robot and UAV projects.
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Size: 1682432 |
Author: snthej |
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Description: 采用ADIS16355经行姿态更新的系统设计方案,提供硬件电路和卡尔曼滤波方法-ADIS16355 by the line attitude updating system design, hardware circuit and Kalman filtering method
Platform: |
Size: 849920 |
Author: Yijie Guo |
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Description: 也是利用ADIS16355进行姿态检测,采用的的ARM7 芯片,对于设计姿态更新系统有帮助-ADIS16355 gesture detection is also used ARM7 chip design attitude updating system
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Size: 625664 |
Author: Yijie Guo |
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Description: 四轴飞行器姿态控制系统设计
四轴飞行器具有不稳定、非线性、强耦合等特性,姿态控制是四轴飞行器飞行控制系统的核心 通过分析四轴飞行器的飞行
原理,根据其数学模型和系统的功能要求,设计了四轴飞行器的姿态控制系统 该系统采用stm32系列32位处理器作为主控制器,使用
ADIS16355惯性测量单元等传感器用于姿态信息检测 系统基于模块化设计的思想,各传感器都使用数字接口进行数据交换,结构简
单 使用PID控制算法进行姿态角的闭环控制,实验结果表明,飞行器能较好的稳定在实验平台上,系统满足四轴飞行器室内飞行姿态
控制的要求。
-Four axis is instability, nonlinear, strong coupling and other features, four axis attitude control is the core of the aircraft flight control system By analyzing the four axis aircraft flight principle, according to its mathematical model and the function of the system, designed the four axis spacecraft attitude control system The system USES stm32 series of 32-bit processor as the main controller, using ADIS16355 sensors such as inertial measurement unit are used in attitude information detection System based on the idea of modular design, each sensor using the digital interface for data exchange, structure is simple For closed-loop control of attitude Angle using PID control algorithm, experimental results show that the craft can better stability in the experimental platform, the system meet the requirements of four axis aircraft flying indoor attitude control.
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Size: 577536 |
Author: 竹林海宝 |
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Description: adis16355驱动程序,spi串口通信(adis16355driver spi serial communications)
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Size: 803840 |
Author: jinshuyu |
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