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针对一种基于DSP的旋翼主动控制捷联姿态系统硬件结构设计方案进行了介绍。该系统主要由ENC-03微机械陀螺仪、MMA7260QT加速度计、HMC1043数字罗盘及TMS320F2808 DSP组成。系统通过增加旋翼主动控制,增强姿态控制的稳定性。
A design scheme of the hardware structure of the AGV attitude control system based on DSP is introduced. The system mainly consists of ENC-03 micromechanical gyroscope, MMA7260QT accelerometer, HMC1043 digital compass and TMS320F2808 DSP. The system enhances the stability of attitude control by increasing the rotor active control.