摘要
简要介绍了一种新型的四旋翼微飞行器的设计方法和整体结构,在此基础上针对此型微飞行器提出了一种新的通过调节电机转速来控制飞行器飞行姿态的控制方法,并设计、制造了飞行器的遥控控制系统。试验表明,此控制方法具有原理简单、易于实现、重量较轻、复杂度较低的优点,有较好的经济性和实用性。
Design method and integration structure of a new four rotor-wings micro air vehicles （MAV） are briefly introduced. Based on this, a new control method for controlling the flying attitude of MAV by adjusting the rotatory speed of the motor is proposed. In the end, a remote control system of the MAV is designed and fabricated. The test results show that this method is simple in principle, easy to accomplish, lighter weight and lower complexity. It is also economic and practical in use.
出处
《航空制造技术》
2006年第5期91-94,共4页
Aeronautical Manufacturing Technology
关键词
微旋翼飞行器
控制
单片机
Rotor-wing micro air vehicle Control Single-chip microprocessor
