Piloting assistance method for aircraft
View Patent ↗The present invention relates to a piloting assistance method for an aircraft, the method consisting in using data from at least one active telemeter sensor (A) in order to construct a sensor safety cordon (B) for avoiding the terrain and obstacles that are overflown. The method; defines and calculates angular sectors (w) over the field of regard facing the pilot; constructs a terrain safety cordon (D) using at least one terrain database (C); for at least some of the angular sectors (w), constructs a hybrid safety cordon (E) that, in each of the angular sectors (w) in question, makes use of the higher of the sensor and terrain safety cordons (B, D); and displays one of the cordons selected from: the hybrid safety cordon (E), the terrain safety cordon (D), and the sensor safety cordon (B).
1. A piloting assistance method for an aircraft, the method comprising:
defining and calculating angular sectors (w) over a field of regard (FOR) facing the aircraft using positioning system information indicative of position of the aircraft;
constructing a sensor safety cordon (B) indicative of an altitude contour above terrain and obstacles in the angular sectors (w) over the field of regard (FOR) using data from an active telemeter sensor (A), using the positioning system information indicative of the position of the aircraft, and using positioning system information indicative of altitude of the aircraft and without using data from a terrain database (C);
constructing a terrain safety cordon (D) indicative of an altitude contour above terrain and obstacles in the angular sectors (w) over the field of regard (FOR) using data from the terrain database (C) including data from an obstacles database (C′) of the terrain database (C) and using the positioning system information indicative of the position of the aircraft and without using data from the active telemeter sensor (A);
constructing a hybrid safety cordon (E) that for each of the angular sectors (w) over the field of regard (FOR) makes use of the higher altitude contour of the sensor and terrain safety cordons (B, D) in the respective angular sector (w); and
displaying on a screen for presentation to the pilot one of the cordons selected from: the hybrid safety cordon (E), the terrain safety cordon (D), and the sensor safety cordon (B).
2. A method according to claim 1 , further comprising:
when one of the sensor safety cordon (B) and the terrain safety cordon (D) is corrupted, selecting the other one of the sensor safety cordon (B) and the terrain safety cordon (D) for displaying on the screen for presentation to the pilot.
3. A method according to claim 1 , wherein the method further includes displaying a hybrid terrain-tracking cordon (ST), said hybrid terrain-tracking cordon (ST) being constructed for a given angular sector (w) over the field of regard (FOR) using the terrain safety cordon (D) in the event of measurements from the active telemeter sensor (A) being absent or lost for the given angular sector (w) or in the event of the given angular sector (w) not being covered by said active telemeter sensor (A).
4. A method according to claim 1 , wherein the method further includes verifying the operating state of locating means and the integrity of the terrain database (C) used for establishing the terrain safety cordon (D), for verifying the operating state of the active telemeter sensor (A) and of a GNSS/AHRS system used for establishing the sensor safety cordon (B), for displaying on the screen only the sensor safety cordon (B) in the event of a failure of the locating means or of corruption of the terrain database (C), and for outputting a terrain alarm in the event of a failure of the locating means or corruption of the terrain database (C) together with a failure of the active telemeter sensor (A).
5. A method according to claim 1 , wherein the method further includes verifying the operating state of locating means and the integrity of the terrain database (C) used for establishing the terrain safety cordon (D), for verifying the operation of the active telemeter sensor (A) and of a GNSS/AHRS system used for establishing the sensor safety cordon (B), and for displaying on the screen only the terrain safety cordon (D) in the event of the active telemeter sensor (A) or the GNSS/AHRS system failing.
6. A method according to claim 1 , wherein the method further includes using a state vector (VE) representing information coming from on-board navigation sensors, in order to construct the terrain safety cordon (D) and the sensor safety cordon (B).
7. A method according to claim 1 , wherein the method further includes displaying on the screen a speed vector (V) symbolizing the aircraft and the position of the aircraft relative to the displayed cordon.
8. A method according to claim 7 , wherein the method further includes constructing a predictive three-dimensional path for following terrain by using a simulated state vector (VE′), the terrain database (C), and a two-dimensional route plotted by the pilot.
9. A method according to claim 8 , wherein the method further includes storing the three-dimensional path together with data relating to the terrain derived from the simulation in such a manner as to cause said path to be followed by an autopilot system.
10. A method according to claim 9 , wherein the method further includes displaying on the screen the terrain safety cordon (D) or the hybrid safety cordon (E) as constructed in real time from the terrain database (C) and the measurements from the active telemeter sensor (A) in order to verify proper operation of the autopilot system.