IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
UP-0030392
(2008-02-13)
|
등록번호 |
US-7777647
(2010-09-06)
|
우선권정보 |
FR-07 01029(2007-02-13) |
발명자
/ 주소 |
- Sallier, Aurélie
- Percier, Julia
- Marty, Nicolas
|
출원인 / 주소 |
|
대리인 / 주소 |
Lowe Hauptman Ham & Berner, LLP
|
인용정보 |
피인용 횟수 :
4 인용 특허 :
5 |
초록
▼
The field of the invention is that of the display in map form of an operating zone of an aircraft on a screen, and more particularly a method of processing topographic data of this operating zone of an aircraft in real time, based on a calculation of radials (R) centred on a reference point (O) defi
The field of the invention is that of the display in map form of an operating zone of an aircraft on a screen, and more particularly a method of processing topographic data of this operating zone of an aircraft in real time, based on a calculation of radials (R) centred on a reference point (O) defining an angular segment of topographic data. According to the invention, the method includes a subdivision of the operating zone to be mapped into a plurality of angular segment sections, each forming an individual zone (3), and an assignment of a processing priority and a refresh frequency specific to each individual zone defined according to a criterion of operational interest of the element to the aircraft.
대표청구항
▼
The invention claimed is: 1. A method of processing topographic data of an operating zone of an aircraft in real time, to display said operating zone in map form on a screen, said processing method comprising: calculating radials centered on a reference point defining an angular segment of topograp
The invention claimed is: 1. A method of processing topographic data of an operating zone of an aircraft in real time, to display said operating zone in map form on a screen, said processing method comprising: calculating radials centered on a reference point defining an angular segment of topographic data, subdividing the operating zone to be mapped into a plurality of sections of angular segments, each forming an individual zone to be mapped, and assigning a priority and of a refresh frequency specific to each individual zone defined according to a criterion of operational interest of an element to the aircraft. 2. The method according to claim 1, comprising geo-referencing of each individual zone. 3. The method according to claim 2, wherein said geo-referencing is obtained by determining, for each of the radials to be calculated for the individual zone, the value of the angle of the radius with a geo-referenced direction. 4. The method according to claim 3, wherein said geo-referencing of an individual zone is obtained by determining geo-referencing coordinates of each of the points forming the peaks of the segment section defining said individual zone. 5. The method according to claim 1, wherein a segment section associated with an individual zone has a geometry that is variable in time, defined according to flight parameter(s) comprising the speed of movement and the rotation speed of the aircraft. 6. The method according to claim 1, wherein each individual zone has an angular aperture of the radials to be calculated for said zone made to correspond to it. 7. The method according to claim 1, wherein tasks associated with the calculation of the radials of the individual zones are managed by means of queues, a queue handling tasks of the same refresh frequency, according to their priority. 8. The method according to claim 1, wherein each individual zone has associated with it a larger associated calculation zone, in order to provide, for this individual zone, data in geographic overlap zones between individual zones, said calculation zone being defined according to flight parameters of the aircraft, in particular its heading and its speed. 9. The method according to claim 1, in which the topographic data is data of terrain elevation type supplied by a database that is onboard or accessible onboard. 10. The method according to claim 1, in which the topographic data is meteorological type data. 11. The method according to claim 2, wherein a segment section associated with an individual zone has a geometry that is variable in time, defined according to flight parameter(s) comprising the speed of movement and the rotation speed of the aircraft. 12. The method according to claim 2, wherein each individual zone has an angular aperture of the radials to be calculated for said zone made to correspond to it. 13. The method according to claim 3, wherein each individual zone has an angular aperture of the radials to be calculated for said zone made to correspond to it. 14. The method according to claim 2, wherein tasks associated with the calculation of the radials of the individual zones are managed by means of queues, a queue handling tasks of the same refresh frequency, according to their priority. 15. The method according to claim 3, wherein tasks associated with the calculation of the radials of the individual zones are managed by means of queues, a queue handling tasks of the same refresh frequency, according to their priority. 16. The method according to claim 4, wherein tasks associated with the calculation of the radials of the individual zones are managed by means of queues, a queue handling tasks of the same refresh frequency, according to their priority. 17. The method according to claim 2, wherein each individual zone has associated with it a larger associated calculation zone, in order to provide, for this individual zone, data in geographic overlap zones between individual zones, said calculation zone being defined according to flight parameters of the aircraft, in particular its heading and its speed. 18. The method according to claim 3, wherein each individual zone has associated with it a larger associated calculation zone, in order to provide, for this individual zone, data in geographic overlap zones between individual zones, said calculation zone being defined according to flight parameters of the aircraft, in particular its heading and its speed. 19. The method according to claim 4, wherein each individual zone has associated with it a larger associated calculation zone, in order to provide, for this individual zone, data in geographic overlap zones between individual zones, said calculation zone being defined according to flight parameters of the aircraft, in particular its heading and its speed. 20. The method according to claim 2, in which the topographic data is data of terrain elevation type supplied by a database that is onboard or accessible onboard. 21. The method according to claim 3, in which the topographic data is data of terrain elevation type supplied by a database that is onboard or accessible onboard. 22. The method according to claim 4, in which the topographic data is data of terrain elevation type supplied by a database that is onboard or accessible onboard.
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