LOW-IMPACT LANDING SYSTEM FOR ROTARY WING AIRCRAFT

Abstract: the invention is a low-impact landing system for a rotary wing aircraft comprising a landing pad having a landing surface for landing the rotary wing aircraft an inclination drive unit on the landing pad to support the landing pad and adjust the horizontal inclination of the landing pad according to a control signal, a ground communication unit for receiving an airframe inclination detection signal detected by an airframe inclination detection unit on the rotary wing aircraft and a drive control unit to control the inclination drive unit according to the airframe inclination detection signal so that each landing gear of the rotary wing aircraft contacts the landing surface of the landing pad at the same timing.

Inventor(s): In Seon OH

CPC Classification: B64F1/36 (Other airport installations (ground installations for de-icing aircraft ))

Search for rejections for patent application number 20250187755