CAJ | 학술논문

针对微小型飞行器带载荷能力差的问题，研发了基于微机电系统（ MEMS）传感器的多集成度自动飞行控制系统，介绍了其硬件组成和结构框图，并对包括空速控制、纵向控制、横向控制的导航算法进行了详细介绍，同时基于自主研发的微小型固定翼飞行器进行了试验验证。试验结果证明，该飞行控制系统可以在指定高度要求下引导微小型飞行器完成期望航迹跟踪，满足日常巡检巡查等任务要求。
침대미소형비행기대재하능력차적문제，연발료기우미궤전계통（ MEMS）전감기적다집성도자동비행공제계통，개소료기경건조성화결구광도，병대포괄공속공제、종향공제、횡향공제적도항산법진행료상세개소，동시기우자주연발적미소형고정익비행기진행료시험험증。시험결과증명，해비행공제계통가이재지정고도요구하인도미소형비행기완성기망항적근종，만족일상순검순사등임무요구。
To compensate the limited payload capability of small unmanned air vehicles ( UAVs ) , an integrated automatic flight control system was developed based on micro-electro-mechanical system ( MEMS) sensors.The hardware composition and structure diagram were introduced,and the navigation algorithm was recommended in detail,which included airspeed control,longi-tudinal control and lateral control.Flight experiments were carried out on a micro self-developed fixed-wing UAV.The experiment results prove that the flight control system can guide the UAV to track the expected path under specified height,which satisfies the desired patrol mission requirements.