FIELD: aviation.
SUBSTANCE: invention relates to designs of equipment suspensions on aircrafts. Platform for use in a compact drone comprises a frame assembly, a transmission unit and shooting unit (1). Frame contains first bracket (2), second bracket (4), third bracket (6) and connecting frame (8) for attachment outside. Shooting unit (1) is fixed on first bracket (2), while first bracket (2) is pivotally connected with second bracket (4), and second bracket (4) is pivotally connected with third bracket (6). Transmission unit comprises first engine (3), which is directly connected with first bracket (2) and activates it for a turn relative to second bracket (4), second engine (5) directly connected with second bracket (4) and actuating it for a motion relative to third bracket (6), and third motor (7) drives third bracket (6) to turn relative to connecting frame (8). Center of gravity of first bracket (2), second bracket (4), third bracket (6) and shooting unit (1) is located, in general, on Z axis of third bracket (6) rotation.
EFFECT: there is achieved higher accuracy of correction of position of the platform.
8 cl, 7 dwg
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Authors
Dates
2016-07-10—Published
2011-09-15—Filed