Control Testbed Design for a Miniature Autonomous Helicopter

摘要：

This paper is a specific description of a miniature autonomous helicopter testbed, namely the SRD-Heli. Airframe and avionics system of the helicopter testbed, including the inertial measurement unit, the digital signal processing and the signal switching and transition, are presented in detail. Some control schemes (including PID control and trajectory linearizaiton control) are introduced briefly to test the SRD-Heli. Experimental results concerning the hovering and forward flight are displayed to verify the performances of the testbed.

关键词： Helicopter Testbed Helicopter Control Avionics System

作者: ZHU Bing WANG Qiang ZHENG Zewei HUO Wei

作者单位: The Seventh Research Division, Beihang University, Beijing 100191, P. R. China Science and Technolog Science and Technology on Aircraft Control Laboratory, Beihang University, Beijing 100191, P. R. Chi

会议类型: 国际会议

会议名称: The 31st Chinese Control Conference(第三十一届中国控制会议)

会议地点: 合肥

会议语种:英文

页码: 4383-4388

在线出版日期: 2012-07-01（万方平台首次上网日期，不代表论文的发表时间）