| 摘要 |
There is provided a multirotor aircraft comprising a platform; and at least two pairs of opposing radial arms extending from the platform, the radial arms supporting at least four internal combustion engine powered rotors, rotating actuators for rotating each of the radial arms about an elongate axis; and a flight controller configured for controlling the rotating actuators, wherein the rotors rotate in the same direction; and the flight controller is configured for yaw control by controlling the rotating actuators to rotate at least one pair of the opposing radial arms in opposing rotational directions. |
