Control system design for rotorcraft-based unmanned aerial vehicles using time-domain system identification

被引:71
作者
Shim, DK [1 ]
Kim, HJ [1 ]
Sastry, S [1 ]
机构
[1] Univ Calif Berkeley, Dept Mech Engn, Berkeley, CA 94720 USA
来源
PROCEEDINGS OF THE 2000 IEEE INTERNATIONAL CONFERENCE ON CONTROL APPLICATIONS | 2000年
关键词
D O I
10.1109/CCA.2000.897539
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper introduces the development of flight control system for rotorcraft-based unmanned aerial vehicle(RUAV). In this research, the linear time-invariant model valid for hover is sought. The system response data is acquired in carefully devised experiment procedure and then a linear time-invariant system model is obtained using time-domain analysis method. The acquired model is used to design feedback controller consisting of inner-loop attitude feedback control, mid-loop velocity feedback control and the outer-loop position control. The proposed controller is implemented on digital onboard computer and tested in a Berkeley RUAV and shows outstanding hovering performance.
引用
收藏
页码:808 / 813
页数:6
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