|
Frame Type |
kg |
Hovering Time min. |
Flight Altitude m |
Design Application |
Battery Type |
Recommended Configurations
| Num. | Motor | ESC | Propeller | Battery | Frame Size | Hovering Time | Load Weight | Total Weight (include load) |
|---|---|---|---|---|---|---|---|---|
| 1 | ||||||||
| 2 | ||||||||
| 3 | ||||||||
| 4 | ||||||||
| 5 | ||||||||
| 6 | ||||||||
| 7 | ||||||||
| 8 |
News and Documents
News [3]：Part of the rapid design algorithm is published as journal article: X. Dai, Q. Quan, J. Ren, and K.-Y. Cai, “An Analytical Design Optimization Method for Electric Propulsion Systems of Multicopter UAVs with Desired Hovering Endurance,” IEEE/ASME Transactions on Mechatronics, vol. 24, no. 1, pp. 228–239, 2019. [PDF], [BibTex]
News [4]：Part of the efficiency optimization algorithm is published as journal article: X. Dai, Q. Quan, J. Ren, and K.-Y. Cai, “Efficiency Optimization and Component Selection for Propulsion Systems of Electric Multicopters. IEEE Transactions on Industrial Electronics, vol. 66, no. 10, pp. 7800–7809, 2019. [PDF], [BibTex]
News [5]：Part of the modeling and simulation method is published as journal article: X. Dai, C. Ke, Q. Quan and K. -Y. Cai, “Simulation Credibility Assessment Methodology With FPGA-based Hardware-in-the-Loop Platform,” IEEE Transactions on Industrial Electronics, vol. 68, no. 4, pp. 3282-3291, 2021. [PDF], [BibTex]
News [6]：Part of the simulation and test method is published as journal article: X. Dai, C. Ke, Q. Quan and K. -Y. Cai, “RFlySim: Automatic test platform for UAV autopilot systems with FPGA-based hardware-in-the-loop simulations,” Aerospace Science and Technology, vol. 114, p. 106727, 2021. [PDF], [BibTex]
