| 摘要 |
<p>#CMT# #/CMT# The system (1) has a guiding unit (3) generating guiding commands to guide a referent aircraft, so that the referent aircraft passes via a waypoint at a required time of arrival (RTA) type passing time. A detection unit (4) detects a risk of collision between the referent and target aircrafts. A selection unit (5) selects the unit (3) during a normal flight situation, in the absence of detection of a risk of collision and selects another guiding unit (2) during a danger situation, when the unit (4) detects the collision risk, where the unit (2) is being selected until the risk subsists. #CMT#USE : #/CMT# System for guiding an aircraft (claimed) e.g. transport aircraft such as civil or military aircraft, during a landing phase of the aircraft on an airport. #CMT#ADVANTAGE : #/CMT# The configuration of the guiding system ensures an arrival time of the aircraft at any waypoints in space e.g. usual point of convergence for the aircraft during a landing phase on an airport, with a desired level of accuracy and a specific level of probability, and optimizes fuel consumption, wear of engines and environmental impact. The guiding system assists an air controller to effectively anticipate the development of the traffic and to more accurately sequence the aircraft, while limiting the risks of conflict between two consecutive aircrafts. #CMT#DESCRIPTION OF DRAWINGS : #/CMT# The drawing shows a schematic block diagram of an aircraft guiding system. 1 : Aircraft guiding system 2, 3 : Guiding units 4 : Detection unit 5 : Selection unit 14 : Visual display unit.</p> |
