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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