Control Testbed Design for a Miniature Autonomous Helicopter
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.
Helicopter Testbed Helicopter Control Avionics System
ZHU Bing WANG Qiang ZHENG Zewei HUO Wei
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
国际会议
The 31st Chinese Control Conference(第三十一届中国控制会议)
合肥
英文
4383-4388
2012-07-01(万方平台首次上网日期,不代表论文的发表时间)