Method and device for preventing aerodynes from colliding with relief obstacles

• US 5,515,286 A
• Filed: 02/13/1995
• Issued: 05/07/1996
• Est. Priority Date: 03/24/1994
• Status: Expired due to Term

• Current Assignee: Sextant Avionique
• Original Assignee: Sextant Avionique
• Inventors: Simon, Georges-Henri
• Primary Examiner(s): Teska, Kevin J.
• Assistant Examiner(s): NGUYEN, TAN QUANG
• Application Number:
  US08/387,236
• Time in Patent Office: 449 Days
• Field of Search: 364/460, 364/461, 364/462, 364/449, 364/451, 364/456, 342/29, 342/32, 342/30, 342/37, 342/357, 342/455, 340/961, 340/963, 340/945, 340/951
• US Class Current: 701/301
• CPC Class Codes: G01C 21/00 Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 measuring distance traversed on the ground by a vehicle G01C22/00; control of position, course, altitude or attitude of vehicles G05D1/00; traffic control systems for road vehicles involving transmission of navigation instructions to the vehicle G08G1/0968
• CPC Class Codes: G05D 1/0646 to follow the profile of undulating ground
• CPC Class Codes: G08G 5/0013 with a ground station
• CPC Class Codes: G08G 5/0082 for monitoring traffic from a ground station radar or analogous systems specially adapted for traffic control G01S13/91
• 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

The method embodying the invention comprises the periodical drawing up and transmission, on board an aerodyne, of a tracking message comprising a code identifying the aerodyne and navigational data, to an air surveillance station for a geographical area, permanent monitoring by said station and reception of tracking messages transmitted by the aerodynes in the vicinity, determination of their respective future paths within said geographical area, detection by said station of the risks of collision of each aerodyne with a relief obstacle, and drawing up by said station of the avoidance commands to be performed by the pilot of the aerodyne and transmission of these commands to the pilot. This method does not implement any specific autonomous system, while providing a high degree of security.

Claims

1. A device for preventing collisions between an aerodyne and obstacles formed by relief of a geographical area flown over by said aerodyne, said device comprising:

a computer, provided in a ground station for air surveillance of said geographical area, said computer being linked up to Hertzian waves communication means and to a geographical data base describing the relief of said geographical area;

data acquisition means, provided in said aerodyne, for automatically and periodically acquiring navigation data representative of a current position and further flight path of said aerodyne, and for drawing up tracking messages each comprising an identification code of said aerodyne and said navigation data associated with a date of acquisition;

Hertzian waves communication means, provided in said aerodyne for sending said tracking messages, said tracking messages being received by the communication means of the ground station when said aerodyne is flying over said geographical area,

display means, provided in said aerodyne, for displaying information sent by the communication means of the ground station and received by the communication means of said aerodyne;

said computer comprising;

means for permanently monitoring said tracking messages received by the communication means of the ground station,

means for identifying said aerodyne with said identification code contained in each of said tracking messages,

means for estimating and localizing in said geographical area the further flight path of said aerodyne, by means of the navigation data contained in each of said tracking messages and said geographical data base, and for determining risks of collisions of said aerodyne with obstacles of relief,

computation means for drawing up avoidance flight commands to be performed by a pilot of said aerodyne so as to prevent said aerodyne from colliding with an obstacle of relief, said computation means using said geographical data base, said estimated further flight path and estimated further flight paths of other aerodynes flying over said geographical area,

means for drawing up avoidance messages comprising a last received tracking message from said aerodyne, an indication on said risks of collision and said avoidance flight commands, said avoidance message being transmitted to said aerodyne and displayed on said display means.

2. The device as claimed in claim 1, wherein a tracking message of said aerodyne comprises:

identification code of said aerodyne,

airspeed, ground speed and vertical velocity,

real position in terms of longitude, latitude and altitude, and

velocity vector thereof.

3. The device as claimed in claim 2, wherein said estimating means estimate said further flight path of said aerodyne by means of the real position and velocity vector provided in a last tracking message received from said aerodyne, and estimate a position said aerodyne will occupy a predetermined period of time later.

4. The device as claimed in claim 3, wherein, if the estimated flight path during said period of time intercepts an obstacle, said computation means determine said avoidance flight commands from the following data:

the real position provided in the last tracking message and the estimated position,

the airspeed and ground speed provided by said last tracking message,

a configuration of the relief between said real position and said estimated position, provided by said geographical data base,

a decision height corresponding to the minimum height for overshooting and deferring a landing, provided by said geographical data base,

respective estimated further flight paths of other aerodynes detected within radioelectric range of said ground station.

5. The device as claimed in claim 2, wherein each of said tracking messages further comprises a starting descent indicator which indicates whether the aerodyne has begun an approach phase to a landing strip, this indicator in said tracking message being used by said computation means to determine which avoidance strategy to apply when a risk of collision is detected.

6. The device as claimed in claim 2, wherein each of said tracking messages further comprises a starting descent indicator which indicates whether the aerodyne has begun an approach phase to a landing strip, this indicator in said tracking message indicating to said computing means that the presence of an obstacle and the distance thereto must be simply signalled in the avoidance message returned.

7. The device as claimed in claim 1, said communication means of said aerodyne comprising:

means for permanently monitoring and receiving avoidance messages transmitted by said ground station, means for selecting said avoidance messages received concerning said aerodyne by means of identification code thereof, means for transmitting said indication on said risks and said avoidance commands to said display means, and means for transmitting an acknowledgement message to said station after one avoidance message being selected by said selecting means.

8. The device as claimed in claim 1, wherein said geographical data base comprises altitudes of a multiplicity of points evenly distributed over the entire geographical area.