电子器件2012，Vol.35Issue(1)：47-51,5.DOI:10.3969/j.issn.1005-9490.2012.01.012
一种基于STM32的航模直升机飞控系统设计
Design of STM32-Based Flying Control System for a Mold Helicopter
摘要
Abstract
A flight control scheme taking STM32 processor as the core and based on a data collecting for multi-sensors and an adaptive PID algorithm for mold helicopter is introduced. The modeling of mold helicopter dynamics under hover and low speed conditions is based on the analyzed of the structure of control system for mold helicopter and the flight attitude control and navigation control is designed. The flight-test data compared with the simulation result showed that the flight control system is feasible and correct.关键词
直升机/飞控系统/适应控制/PIDKey words
helicopter/flight control system/adaptive control/PID分类
航空航天引用本文复制引用
陈贻国,钱金芳,潘日敏..一种基于STM32的航模直升机飞控系统设计[J].电子器件,2012,35(1):47-51,5.基金项目
浙江省大学生科技创新活动计划(新苗人才计划)项目(2010R404018) （新苗人才计划）
