Method and device for preventing collisions with the ground for an aircraft

• US 5,638,282 A
• Filed: 10/13/1995
• Issued: 06/10/1997
• Est. Priority Date: 04/07/1992
• Status: Expired due to Term

• Current Assignee: Dassault Electronique
• Original Assignee: Dassault Electronique
• Inventors: Hunot, Anne-Marie, Chazelle, Xavier, Lepere, Gerard
• Primary Examiner(s): ZANELLI, MICHAEL J
• Application Number:
  US08/542,645
• Time in Patent Office: 606 Days
• Field of Search: 364/461, 364/449, 364/456, 364/434, 364/433, 340/963, 340/967, 340/970, 342/64, 342/65, 342/29, 342/357
• US Class Current: 701/301
• CPC Class Codes: G01C 21/005 with correlation of navigation data from several sources, e.g. map or contour matching G01C21/30 takes precedence
• CPC Class Codes: G01S 13/935 for terrain-avoidance
• CPC Class Codes: G01S 19/15 Aircraft landing systems
• CPC Class Codes: G01S 19/47 the supplementary measurement being an inertial measurement, e.g. tightly coupled inertial
• CPC Class Codes: G05D 1/0646 to follow the profile of undulating ground
• CPC Class Codes: G05D 1/0653 during a phase of take-off or landing
• CPC Class Codes: G08G 5/0013 with a ground station
• CPC Class Codes: G08G 5/0086 for monitoring terrain radar or analogous systems specially adapted for terrain avoidance G01S13/935
• CPC Class Codes: G08G 5/045 Navigation or guidance aids, e.g. determination of anti-collision manoeuvers radar or analogous systems specially adapted for anti-collision between aircraft G01S13/933

Abstract

A mass memory stores a data base representing at least a substantial part of the terrestrial globe, in accordance with a grid configuration on several levels, said grid configuration being in particular more precise in the vicinity of an airport. Status indications are received representing the position of the aircraft with two horizontal components, and the altitude, and the velocity and acceleration vectors of the aircraft, as well as control indications coming from the flight deck. In accordance with the horizontal components of the position of the aircraft, a temporary local map is transferred into a fast access memory, on the basis of which map, an altitude envelope of the terrain is established in the zone where the aircraft is travelling. Anticollision processing make it possible to establish an alarm if the relation between a protection field and the altitude envelope meets a first condition which is defined at least partly by the control indications. The device has application as an aid for aerial navigation.

Claims

1. In an aerial navigation aid device, the improvement comprising:

(a) mass memory means for storing a data base representing at least a substantial part of the terrestrial globe, in a cutout form comprising a grid configuration having at least one level of resolution, each grid being associated with at least one data item representing the maximum altitude inside the grid, said data base having sets of contiguous grids, accessible in accordance with a system of addressing by two horizontal coordinates;

(b) input means for receiving status indications representing the position of the aircraft with two horizontal components and the altitude, and its velocity vector, defining the present flight path of the aircraft;

(c) a fast access working memory;

(d) management means, responsive to said status indications, for accessing said data base to maintain a temporary local map in said fast access working memory, said temporary local map corresponding to the zone wherein the aircraft is traveling, and defining a ground altitude envelope of the terrain in said zone;

(e) anti-collision means for determining whether the present flight path matches first and second anti-collision laws in relationship with said ground altitude envelope; and

(f) alarm means capable of selectively establishing a first alarm in accordance with a first condition, which includes the fact that said first anti-collision law is violated, and a second alarm in accordance with a second condition, which includes the fact that said second anti-collision law is violated.

2. A device according to claim 1, wherein the resolution of said temporary local map is variable, with a higher resolution being provided for, at least in the vicinity of airport zones.

3. A device according to claim 1, wherein said first and second anti-collision laws are specific to the aircraft.

4. A device according to claim 1, wherein the altitude in said position data comprises baro-inertial altitude.

5. A device according to claim 4, wherein the altitude in said position data comprises altitude data from an independent radionavigational source.

6. A device according to claim 1, wherein said two horizontal components in said position data are derived from the combination of a radionavigational instrument with an inertial on-board instrument.

7. A device according to claim 1, wherein said input means are arranged for receiving velocity vector data and acceleration vector data from on-board inertial instruments, and said anti-collision means takes account of said velocity vector data and acceleration vector data.

8. A device according to claim 1, wherein said input means are arranged for further receiving the attitude angles of the aircraft from on-board inertial instruments, and said anti-collision means takes account of said attitude angles of the aircraft.

9. A device according to claim 8, wherein said first and second anti-collision laws take account of the fact that the aircraft is in a straight line or is in a turn.

10. A device according to claim 9, wherein the attitude angles are derived from an inertial unit installed on-board the aircraft.

11. A device according to claim 1, wherein said first anti-collision law corresponds to an extrapolated piloting flight path for pulling-up with a virtually maximum amplitude after a brief delay, and said second anti-collision law corresponds to an extrapolated piloting flight path for pulling-up with a virtually maximum amplitude after a longer delay, whereby said first anti-collision law corresponds to a short term danger of ground collision, while said second anti-collision law corresponds to a medium term danger of ground collision.

12. A device according to claim 1, wherein said input means comprises first input means for receiving a first set of said two horizontal components from on-board inertial instruments, second input means for receiving a second set of said two horizontal components from an independent radionavigational source, and means for combining such two sets of said two horizontal components into a pair of enhanced precision horizontal components, for use in said management means.

13. A device according to claim 12, wherein said input means comprises third input means for receiving height to ground data, and means for influencing the operation of said anti-collision means in accordance with said height to ground data.

14. A device according to claim 13, wherein said independent radionavigational source is a GPS receiver.

15. A device according to claim 12, wherein said independent radionavigational source is a GPS receiver.

16. A device according to claim 12, wherein said means for combining comprises a Kalman filter.