產品資訊
產品資訊
產品規格
裝置質量
|
6.2 kg
|
高度(支架底面到頂端)
|
45 cm
|
長度(配重到前面螺旋槳)
|
127 cm
|
直升機質量
|
1.15 kg
|
直升機機身長度
|
49.8 cm
|
底座尺寸(W × L)
|
17.5 cm × 17.5 cm
|
仰俯和翻滾編碼器精度(倍頻後)
|
4096 counts/rev
|
旋轉編碼器精度(倍頻後)
|
8192 counts/rev
|
翻滾角
|
64 (±32.0 deg)
|
俯仰角範圍
|
63.5 deg
|
旋轉角範圍
|
360 deg
|
螺旋槳直徑
|
20.3 cm
|
螺旋槳螺距
|
15.2 cm
|
電機電樞電阻
|
0.83 Ω
|
電機電流/力矩常數
|
0.0182 Nm/A
|
應用領域
航空動力學
研究論文
近期論文收集
Zhu, X., Li, D. Robust fault estimation for a 3-DOF helicopter considering actuator saturation. Mechanical Systems and Sign, Processing, Vol. 15 (2020).
M. Nkemdirim, S. Dharan, H. Chaoui, S. Miah.LQR control of a 3-DOF helicopter system.Journal Proceedings: International Journal of Dynamics and Control(2021)
N. M. Vijayan, M. S. Johnson, J. Jacob.Convex-Optimization-based Constrained Control Strategy for 3-DOF Tandem Helicopter using Feedback Linearization.Journal Proceedings: Journal of Optimization Theory and Applications(2021)
Kumar Abhinav; S.J Mija.Observer Based Sliding Mode Control for 3 DOF Helicopter System.2021 International Conference on Intelligent Technologies (CONIT)(2021)
C. Lin, B. Jiang, K. Zhang, S. X. Ding.Hierarchical Structure-Based Fault-Tolerant Tracking Control of Multiple 3-DOF Laboratory Helicopters.Journal Proceedings: IEEE Transactions on Systems, Man, and Cybernetics: Systems(2021)
J. Kim; W.H. Ko; P. R. Kumar.Cyber-Security through Dynamic Watermarking for 2-rotor Aerial Vehicle Flight Control Systems.Conference Proceedings: 2021 International Conference on Unmanned Aircraft Systems (ICUAS)(2021)
Hamid Reza Karimi.Editorial: Special Issue on Automation in Mechatronic and Robotic Systems – Advanced Perception, Planning and Control.Transactions of the Institute of Measurement and Control(2021)