Method For Estimating An Aircraft Distance Taking Into Account Air Navigation Constraints

• US 20070219705A1
• Filed: 03/22/2005
• Published: 09/20/2007
• Est. Priority Date: 04/20/2004
• Status: Active Grant

• Current Assignee: Thales SA
• Original Assignee: Thales SA
• Inventors: Marty, Nicolas, Bitar, Elias
• Granted Patent: US 7,634,335 B2
• Time in Patent Office: Days
• US Class Current: 701/200
• CPC Class Codes: G01C 21/005 with correlation of navigation data from several sources, e.g. map or contour matching G01C21/30 takes precedence

Abstract

This method uses for the estimation of a distance, a propagation distance transform considering only the paths which are both accessible to the aircraft taking account of its vertical flight profile and complying with air regulations. The propagated distance D_p is accompanied by a propagated altitude A_p which at all points follows the vertical flight profile of the aircraft, whilst being greater than the altitudes of these points and complying with the air regulation constraints at these points. This is obtained by subjecting the propagation to compliance with the vertical flight profile of the aircraft, constraints of the elevations of the points of the relief and air regulation constraints.

Claims

1. A method of estimating distances of points in a map extracted from a terrain elevation database, with respect to an aircraft subjected, to dynamic altitude restrictions prohibiting it from crossing certain reliefs on the map that are too high whose configuration varies according to the vertical flight profile imposed upon it and, to constraints and restrictions coming from air navigation regulations;

the terrain elevation database having a set of points each referenced by an elevation, a latitude and a longitude, and corresponding to the regular meshing of a location grid;

the methods comprising the steps of implementing, on the image constituted by the elements of the database which correspond to the map and are disposed in lines and columns in order of values of latitude and longitude, a propagation distance transform assimilating the distances of the different points of the image with respect to a source point placed close to the aircraft, to the shortest joining paths compatible with the dynamic altitude restrictions of the aircraft, and with air navigation constraints and restrictions.

2. The method according to claim 1, wherein the air navigation constraints and restrictions are translated into local altitude constraints for each point in the terrain elevation database, the propagation distance transform considering only the joining paths accessible to the aircraft, of which all points comply with local altitude constraints.

3. The method according to claim 2, wherein the propagation distance transform propagates over the points of the image constituted by elements of the terrain elevation database, the altitudes which the aircraft would take at these point after having traveled joining paths of minimum length in compliance with its vertical flight profile, called the propagated altitudes, and measurements of distance from the aircraft called the propagated distances, a propagated distance at a point being taken into account for a distance estimation only if the associated propagated altitude is greater than the elevation of the point in question appearing in the terrain elevation database and complies with the local altitude constraints.

4. The method according to claim 2, wherein the local altitude constraints at each point in the terrain elevation database are expressed by minimum and maximum authorized altitude attributes associated with the elevation value of the terrain at that point.

5. The method according to claim 2, wherein the points of the terrain elevation database are allocated with a binary propagation attribute authorizing or not authorizing, depending on its value, the propagation to the point in question of the propagation distance transform.

6. The method according to claim 2, wherein local altitude constraints are associated with the points of the terrain elevation database for creating virtual obstacles in line form around assemblies formed by destination points uniquely accessible by corridors imposed by air regulations, their imposed access corridors and the sides of the angular access sectors to these corridors, said virtual obstacles in line form constituting around these points lobster pot shaped guidance boundaries, forcing the propagation distance transform to consider only joining paths actually passing through the imposed access corridors.

7. The method according to claim 6, wherein the ends of the virtual obstacles in line form are turned back towards the outside in the form of loops and constitute, at the entrance to the access corridors, lateral access roundabouts taking account of the limited turning radius of the aircraft.

8. The method according to claim 6, wherein binary propagation attributes of non authorized value are associated with the points of the terrain elevation database belonging to virtual obstacles in line form.

9. The method according to claim 6, wherein imposed minimum altitude attributes of infinite value are associated with the points of the terrain elevation database belonging to the virtual obstacles in line form.

10. The method according to claim 5, wherein the propagation distance transform analyzes a point of the image constituted by elements of the terrain elevation database only after having verified that it has not been associated with a propagation attribute of non authorized value.

11. The method according to claim 4, wherein the distance transform takes into consideration for a point the highest of the elevation value and the minimum imposed altitude value instead and in place of the elevation of the point.

12. The method according to claim 1, wherein, when a maximum authorized altitude attribute is associated with a point in the terrain elevation database and the propagation distance transform propagates over the points of the image constituted by elements of the terrain elevation database, an altitude which is the one which the aircraft would take after having traveled a joining path of minimum length whilst complying with its vertical flight profile, and a distance measurement from the aircraft, the distance propagated at a point is taken into account for a distance estimation only if the associated propagated altitude is greater than the elevation of the point in question appearing in the terrain elevation database and less than the value of the authorized maximum altitude attribute.