Design of UAV Downwash Airflow Field Detection System Based on Strain Effect Principle
Abstract
:1. Introduction
2. Measurement Principle of Acquisition System
3. Strain Simulation Analysis and Parameter Determination of Acquisition System
3.1. Finite Element Modeling and One-Way Fluid-Solid Coupling Analysis
3.1.1. Establishment of Rotor Finite Element Model
3.1.2. Regional Boundary Setting and One-Way Fluid-Solid Coupling Analysis
3.2. Acquisition System Simulation Analysis and Parameter Determination
3.2.1. Simulation of the Downwash Airflow Field under the Rotor
3.2.2. Flexible Detection Structure Acquisition Card Simulation Analysis and Parameter Determination
4. Experiment Preparation and Test Design
4.1. Material and Layout
4.2. Experiment Design
4.3. Influence Test and Analysis of Difference in Flexible Structure Acquisition System
4.4. Calibration Test and Result Analysis of the Flexible Structure Acquisition System
4.5. Application Test
5. Results and Discussion
5.1. Testing Results of the Flexible Structure Acquisition System
5.2. Analysis of the Wind Field in 3D Shape of the Flexible Structure Acquisition System
5.3. Analysis and Discussion on 3D Shape of Wind Field
6. Conclusions
Author Contributions
Funding
Conflicts of Interest
References
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Acquisition System Number | Single Bridge Voltage Output Value/(mv) | Acquisition System Number | Half Bridge Voltage Output Value/(mv) | Acquisition System Number | Full Bridge Voltage Output Value/(mv) |
---|---|---|---|---|---|
D1 | 120 | B1 | 234 | Q1 | 469 |
D2 | 126 | B2 | 240 | Q2 | 475 |
D3 | 119 | B3 | 235 | Q3 | 480 |
D4 | 112 | B4 | 246 | Q4 | 468 |
D5 | 116 | B5 | 241 | Q5 | 489 |
D6 | 118 | B6 | 239 | Q6 | 475 |
D7 | 123 | B7 | 236 | Q7 | 471 |
D8 | 125 | B8 | 243 | Q8 | 469 |
D9 | 120 | B9 | 241 | Q9 | 481 |
Parameter | Data |
---|---|
Motor model | X4114KV370 |
Distance between axes (mm) | 800 |
Rotor model | 1555 |
Rotor diameter (mm) | 380 |
Number of rotors (unit) | 6 |
Rotor speed (rpm) | 2500 |
Height | W | C | RMSE | emax |
---|---|---|---|---|
0.4 m | 0.648 | 0.6397 | 0.2238 | 16.07% |
0.7 m | 0.831 | 0.8219 | 0.1725 | 9.91% |
1.0 m | 0.960 | 0.9367 | 0.1246 | 5.61% |
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Wu, Y.; Qi, L.; Zhang, H.; Musiu, E.M.; Yang, Z.; Wang, P. Design of UAV Downwash Airflow Field Detection System Based on Strain Effect Principle. Sensors 2019, 19, 2630. https://doi.org/10.3390/s19112630
Wu Y, Qi L, Zhang H, Musiu EM, Yang Z, Wang P. Design of UAV Downwash Airflow Field Detection System Based on Strain Effect Principle. Sensors. 2019; 19(11):2630. https://doi.org/10.3390/s19112630
Chicago/Turabian StyleWu, Yalei, Lijun Qi, Hao Zhang, Elizabeth M. Musiu, Zepeng Yang, and Pei Wang. 2019. "Design of UAV Downwash Airflow Field Detection System Based on Strain Effect Principle" Sensors 19, no. 11: 2630. https://doi.org/10.3390/s19112630
APA StyleWu, Y., Qi, L., Zhang, H., Musiu, E. M., Yang, Z., & Wang, P. (2019). Design of UAV Downwash Airflow Field Detection System Based on Strain Effect Principle. Sensors, 19(11), 2630. https://doi.org/10.3390/s19112630