摘要:
A method for verifying the coherence of the takeoff parameters of an aircraft from an airport with an available runway length at the moment of takeoff comprises a step (E20) of identifying a takeoff runway and a step (E30) of validating the takeoff parameters with a view to authorizing takeoff of the aircraft if the takeoff distance is shorter than the remaining runway length associated with the identified takeoff runway.Use to make takeoff of an aircraft from an airport safe.
摘要:
A method for verifying coherence of takeoff parameters of an aircraft from an airport with an available runway length at a moment of takeoff comprises a step of identifying a takeoff runway and a step of validating takeoff parameters with a view to authorizing takeoff of the aircraft if the takeoff distance is shorter than the remaining runway length associated with the identified takeoff runway.
摘要:
A method for detecting an error in input of one of the takeoff parameters into a flight management system includes a step of calculating a limit value based on one or more takeoff parameters input into the flight management system. The method further includes a step of comparing the calculated limit value with characteristic takeoff values.
摘要:
A method for detecting an error in input of one of the takeoff parameters into a flight management system includes a step of calculating a limit value based on one or more takeoff parameters input into the flight management system. The method further includes a step of comparing the calculated limit value with characteristic takeoff values.
摘要:
The device (1) comprises means (3) for determining the current values of flight parameters of the airplane, means (4) for determining, at least with the aid of said current values, an approach distance which corresponds to a distance in a horizontal plane between the current position of the airplane and a position of contact with the ground, and display means (6) for presenting this approach distance on a screen (8).
摘要:
A method and device for aiding the piloting of an airplane includes: (1) determining current values of flight parameters of the airplane, (2) determining, with the aid of the current values, an approach distance that corresponds to a distance in a horizontal plane between the current position of the airplane and a position of contact with the ground, and (3) presenting the approach distance on a screen.
摘要:
System for aiding the piloting of an aircraft during the approach to a runway with a view to a landing. The system (1) comprises information sources (3) able to provide information relating to the aircraft and to its environment, a computation unit (4) which determines, with the aid of information provided by the information sources (3), an energy reference profile which preferably comprises a trajectory reference profile and a speed reference profile and which is intended to allow the aircraft to regain a stabilized approach trajectory, if it follows this reference profile, means of monitoring (7) for verifying that the aircraft is indeed following said reference profile, and means of indication (6) which supply the pilot with piloting indications at least to make it possible to pilot the aircraft in such a way that it always follows said reference profile.
摘要:
A system for aiding the piloting of an aircraft during a runway approach includes an information source that provides information relating to the aircraft and its environment. A computation unit determines, with the aid of information provided by the information source, an energy reference profile having a trajectory reference profile and a speed reference profile that allows the aircraft to regain a stabilized approach trajectory, if it follows the reference profile. A monitor verifies that the aircraft is following the reference profile. An indicator supplies the pilot with piloting indications for piloting the aircraft so as to follow the reference profile.
摘要:
The inventive flight control assisting device comprises first means (4) for determining the actual aircraft flight conditions, second means (5) for determining, with the aid of said actual flight conditions and a predetermined pattern, a minimum approaching distance corresponding to a minimum distance between projections on the horizontal plane of the aircraft actual position and a touch-down point when said aircraft moves downwards and decelerates according to an optimised approach in such a way that stabilised approaching conditions are attained, and display means (7) for displaying at least said minimum approaching distance on a navigation screen (9) in the form of a first circular arc focused on a position relative to the aircraft which displays the touch-down position.
摘要:
A terrain avoidance method and system for an aircraft includes a collision alarm device and an auto-pilot device including a first determination unit for determining a climbing order with optimal slope for the aircraft, a checking unit for checking whether a first altitude gain at the relief, by applying the optimal slope climbing order, is sufficient for clearing said relief, a finding unit for finding if at least one heading variation value exists, for which the corresponding altitude gain is sufficient to clear the relief, and a switching and calculating unit for applying to the aircraft, if the first altitude gain is sufficient, an optimal slope climbing order with an order to maintain the current heading and, if the first altitude gain is insufficient, a particular climbing order sufficient to clear the relief, with a heading order which corresponds to the selected heading variation value.