Simplified Quadcopter Simulation Model for Spike-based Hardware PID Controller using SystemC-AMS

被引：4

作者：

Mie, Shunsuke ^{[1
]}

Okuyama, Yuichi ^{[1
]}

Saito, Hiroaki ^{[1
]}

机构：

[1] Univ Aizu, Grad Sch Comp Sci & Engn, Aizu Wakamatsu, Fukushima, Japan

来源：

2018 IEEE 12TH INTERNATIONAL SYMPOSIUM ON EMBEDDED MULTICORE/MANY-CORE SYSTEMS-ON-CHIP (MCSOC 2018) | 2018年

关键词：

Quadcopter; Modeling; FPGA; PID Control; Analog and Mixed-Signal Simulation;

D O I：

10.1109/MCSoC2018.2018.00016

中图分类号：

TP3 [计算技术、计算机技术];

学科分类号：

0812 ;

摘要：

In this research, we employ spike-based PID controller for Quadcopter control. Quadcopters control their attitude by proportionalintegralderivative (PID) controller for four rotors. General hardware controllers use fixed point computations for PID that consume hardware resources. On the other hand, spike-based PID controller can reduce hardware cost compared with using fixed-point ones. For feasibility tests, we implemented (1) spike-based hardware PID controller for quadcopter attitude control, and (2) an analog-digital mixed simulator for single axis quadcopter model using SystemC-AMS. As a result, we reduced FPG

引用

页码：23 / 27

页数：5

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