| 摘要 |
Lift offset management and control systems (20) are provided for a rotorcraft (1) including main rotor (5) and auxiliary propulsor assemblies (6), the main rotor assembly (1) including first (50) and second (51) rotors disposed to oppositely rotate relative to an airframe (2) about a same rotational axis (RA), and sensors (30) disposed to generate hub moment, tip clearance and lift offset data of the main rotor assembly (5). |
