| 摘要 |
<p>The aircraft has a sling fastened to an airframe via a carrier structure. A local transverse vertical plane is provided with a fastening point, and is parallel to a yaw axis and a pitch axis of the aircraft. A local longitudinal vertical plane intersects with the local transverse vertical plane at a vertical axis of the aircraft. A piloting assistance device provided with a main determination unit for determining two main angles. A display unit is provided with a display screen (31) for quantitatively displaying the two main angles. An independent claim is also included for a method for assisting piloting of an aircraft.</p> |
