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1.机架是上一届准备国赛前买的,电机是空心杯(2000转/min) ,电池是11.1V的航模电池 2.采用2块msp430f149最小系统做飞控板,一块用来姿态控制,一块用来完成题目要求,两者之间通过串口通信 3.陀螺仪用的是MPU9150(九轴),自带有地磁传感器,不需要再加地磁传感器 4.数据融合是靠MPU9150的内部DMP处理输出(该部分程序时移植32单片机的,针对430的时钟频率对该部分程序做了一些调整) 5.姿态控制算法是PID-1 rack is the last before the country ready to buy, the motor is a hollow cup (2000 rpm/min), the model aircraft battery is 11.1V battery 2 uses two msp430f149 minimum system do fly control panels, for attitude control of a piece of used to complete the questions asked, through serial communication between the two 3 gyroscope using MPU9150 (nine-axis), comes with a geomagnetic sensor, no plus geomagnetic sensor 4 Data fusion is the process by internal DMP output MPU9150 the (transplant when the part of the program 32 microcontroller, the clock frequency for the section 430 program made ​ ​ some adjustments) 5. attitude PID control algorithm is
Date : 2025-12-24 Size : 404kb User : wanggui
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