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Алгоритмы искусственного интеллекта для тяжелых беспилотных воздушных судов
Measurement results Before and After Propeller Pitch Adjustment Based on Current Draw
Motor RPM = constant 2800 RPM | Initial Stage | Final Stage |
ESC Current 1, A | 54 | 79 |
ESC Current 2, A | 53 | 79 |
ESC Current 3, A | 55 | 80 |
ESC Current 4, A | 54 | 79 |
Propeller Pitch 1 | 8 | 12 |
Propeller Pitch 2 | 8 | 12 |
Propeller Pitch 3 | 8 | 12 |
Propeller Pitch 4 | 8 | 12 |
