| 摘要 |
#CMT# #/CMT# The method involves calculating a final approach segment (208) in a reduced engine speed of an air-ship (200), and calculating a landing segment (209) preparing a gas delivering potential. The air-ship is enslaved in thrust and speed on the final approach segment and the landing segment. Position of an impact point (205) is automatically monitored on a runway (216) of an airport by evaluating position and speed an impact with respect to a current speed of the air-ship, where the evaluation is propagated until the runway. #CMT#USE : #/CMT# Method for calculating an approach path of an air-ship i.e. airbus aircraft, towards a runway of an airport. #CMT#ADVANTAGE : #/CMT# The method increases sound comfort at the level of frontage resident and at the level of the passengers, reduces consumption of fuel to reduce pollutants in layer bases, and reduces cost of flight. The method ensures controlling of a constant speed adapted to landing without disengagement risks, and eliminates the need for modifying software part of flight management system, automatic pilot or auto-throttle. #CMT#DESCRIPTION OF DRAWINGS : #/CMT# The drawing shows a schematic view of an approach path calculated by a calculating method. 200 : Air-ship 205 : Impact point 208 : Final approach segment 209 : Landing segment 216 : Runway. |
