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Attitude and heading refernce system I-AHRS for the EFIGENIA autonomous unmanned aerial vehicles UAV based on MEMS sensor and a neural network strategy for attitude estimation

机译:基于MEMS传感器和神经网络姿态估计的EFIGENIA无人机姿态航向参考系统I-AHRS

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For the autonomous flight, navigation, guidance and control of the EFIGENIA Unmanned Aerial Vehicle it is essential to have high performance 6-DOF attitude and heading reference system measurements. This paper presents the design and development of a real-time intelligent attitude and heading reference system I-AHRS, as in the hardware, as in the intelligent digital neural network software scheme, analysis, design and construction for the orientation calculation for the EFIGENIA EJ-1B MOZART and the EFIGENIA EJ-2B MARIA Autonomous Unmanned Aerial Vehicles UAVs. The EFIGENIA I-AHRS consists of three MEMS accelerometers, three MEMS rate-gyros and three magnetoresistive transducers that send its outputs to a digital neural network in which is possible to develop a strategy for attitude estimation. Additionally it is well known that the Kalman Filter is an option as multi-sensor data fusion and integration, however it has some adaptability limitations. In this paper, FPGA reconfigurable hardware digital neural network architecture is presented and utilized to replace the Kalman Filter in the integration of MEMS IMU inertial sensors signals and the Magneto resistive sensors.
机译:对于EFIGENIA无人机的自主飞行,导航,制导和控制,必须具有高性能的6自由度姿态和航向参考系统测量。本文介绍了实时智能姿态和航向参考系统I-AHRS的设计和开发,如在硬件中,在智能数字神经网络软件中的方案,分析,设计和构造,用于EFIGENIA EJ的定向计算-1B MOZART和EFIGENIA EJ-2B MARIA自主无人机。 EFIGENIA I-AHRS由三个MEMS加速度计,三个MEMS速率陀螺仪和三个磁阻传感器组成,这些传感器将其输出发送到数字神经网络,在其中可以开发一种姿态估计策略。另外,众所周知,卡尔曼滤波器是多传感器数据融合和集成的一种选择,但是它具有一些适应性限制。在本文中,提出了FPGA可重构硬件数字神经网络架构,并将其用于取代MEMS IMU惯性传感器信号和磁阻传感器的集成中的卡尔曼滤波器。

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