| 摘要 |
A system for rigging a control surface (12) of an aircraft, wherein the control surface (12) is movable relative to a reference structure (4) of the aircraft (2) by means of at least one actuator (18), comprises a mobile control unit having being connectable to at least one actuator (18), an input means for commanding a deflection of the control surface (12), and an optical rigging apparatus having a first rigging component (20) and a second rigging component (22). The first rigging component (20) is adapted for being mounted on a reference structure to which the control surface (12) is swivably attached and the second rigging component (22) is adapted for being mounted on the control surface itself (12). Thereby an accurate rigging may be conducted with a clearly reduced number of personnel and a clearly reduced time for completion. |
