CAJ | 학술논문

四轴飞行器作为一种飞行稳定、能任意角度灵活移动的飞行器,应用越来越广泛.本文设计的四轴飞行器是在动力学建模的基础上,通过陀螺仪与加速度传感器检测飞行器的平衡状态,由超声波电路检测飞行器飞行高度,结合无线收发电路采集的数据,应用PID算法控制飞行器的飞行姿态.实验结果表明设计的飞行器控制系统能较好地执行飞行任务.
사축비행기작위일충비행은정、능임의각도령활이동적비행기,응용월래월엄범.본문설계적사축비행기시재동역학건모적기출상,통과타라의여가속도전감기검측비행기적평형상태,유초성파전로검측비행기비행고도,결합무선수발전로채집적수거,응용PID산법공제비행기적비행자태.실험결과표명설계적비행기공제계통능교호지집행비행임무.
Quadrotor is more and more widely applied because its flight is stable and its aircraft angle is flexibly mobile. Quadrotor is designed in this paper on the basis of the dynamics modeling. The balanced state of the air?craft by the gyro is detected with the acceleration sensor, which is detected by the ultrasonic circuit aircraft flight height, combined with a wireless transceiver circuit acquisition data, and application PID algorithm to con?trol the aircraft flight. Experimental results show that: the design of the aircraft can achieve the mission to meet the design requirements.