Research Article
Design of Flight Control System for a Novel Tilt-Rotor UAV
Table 2
Description of the channel throttles.
| | Channels | Definitions |
| | Vertical | : motors stop working. : the vertical maximum thrust is generated | | Pitch | is the maximum maneuvering capability of making aircraft raise up (or down) its nose. means no pitching control | | Roll | is the maximum maneuvering capability of rolling left (or right). means no rolling control | | Yaw | is the maximum maneuvering capability of yawing left (or right). means no yawing control |
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