Method for assistance with the construction and validation of an avionics platform

• US 8,818,767 B2
• Filed: 05/17/2010
• Issued: 08/26/2014
• Est. Priority Date: 05/18/2009
• Status: Expired due to Fees

• Current Assignee: Airbus Operations (European Aeronautic Defence and Space Company EADS NV)
• Original Assignee: Airbus Operations SAS (Airbus SE)
• Inventors: Minot, Frdric
• Primary Examiner(s): Saxena, Akash
• Application Number:
  US12/781,273
• Publication Number:
  US 20100292979A1
• Time in Patent Office: 1,562 Days
• Field of Search: 703/1, 703/21, 703/13, 710/305, 701/3
• US Class Current: 703/1
• CPC Class Codes: G06F 30/15 Vehicle, aircraft or watercraft design

Abstract

A method for assisting the construction and validation of an avionics platform uses, on the one hand, a functional description of the platform using avionics functions, software modules suitable for executing these functions, and functional link occurrences between these modules and, on the other hand, a material description of this platform using calculation or communication items of equipment and physical links between these equipment. The method according to the invention enables to generate paths between the various items of equipment by using direct physical links and/or physical links belonging to one or more network(s), and subsequently to associate at least one such path to be each functional link occurrence. It also enables to associate to each software module an item of equipment adapted to host it.

Claims

1. A method for assisting the construction of an avionics platform, using a tool including:

a first functional database in which is stored a functional description of the platform,

a second material database in which is stored a material description of the platform, and

a workstation, linked to the first and second databases,

wherein said method is to implement a set of avionics functions, where each avionics function comprises one or more software modules, and where any two software modules can exchange messages based on a link, known as a functional link occurrence, and

wherein said avionics platform includes;

items of equipment linked together by unidirectional or bidirectional physical links belonging to different types of networks, and

paths enabling linking of said equipment, where each path consists of one of the following;

a single direct physical link between a source item of equipment and a destination item of equipment,

a first physical link between said source item of equipment and a first network node,

a second physical link between said destination item of equipment and a second network node, and

at least a third physical link between said first and second nodes,

the method comprising;

associating each software module with an item of equipment onto which said software module is intended to be hosted;

for each functional link occurrence, providing to the workstation a list of all possible topological paths enabling a first item of equipment and a second item of equipment respectively hosting corresponding software modules to be linked;

receiving from the workstation a selection of one of the topological paths from the list;

associating each functional link occurrence with a corresponding selected topological path to let pass through each functional link occurrence the messages of the functional link occurrence;

checking each item of equipment as to whether each item of equipment has sufficient material resources to allow execution of the software module or modules associated therewith; and

generating an implementation file listing all of the items of equipment and providing;

for each software module, the item of equipment associated therewith, if each equipment has sufficient material resources as determined by the checking, and

for each functional link occurrence over which two software modules exchange messages, the at least one path associated therewith.

2. The method for assisting the construction of an avionics platform according to claim 1, further comprising:

checking for each item of equipment, as to whether the connection resources of connectors of each item of equipment are sufficient to receive the topological paths associated with the functional links of the software modules associated with each item of equipment.

3. The method for assisting the construction of an avionics platform according to claim 1, wherein the physical links are one of a first type enabling an item of equipment to be linked in unidirectional fashion to one sole other item of equipment, a second type enabling an item of equipment to be linked in unidirectional fashion to several other items of equipment, a third type enabling two items of equipment to be linked in bidirectional fashion, or a fourth type enabling multiple items of equipment to be linked in bidirectional fashion.

4. The method for assisting the construction of an avionics platform according to claim 3, further comprising:

associating each connector of an item of equipment with connection resources, where each connection resource is capable of receiving a physical link of the first, second, third, or fourth type.

9. The method for assisting the construction of an avionics platform according to claim 1, wherein if one or more of the material resources and connection resources are sufficient, then said avionics platform is implemented using these resources.

10. A tool for assisting the construction of an avionics platform, comprising:

a first database in which is stored a functional description of said avionics platform,

a second database in which is stored a material description of said avionics platform, and

a workstation linked to the first and second databases, where said workstation comprises a processor configured to implement the method according to claim 1.

11. The tool for assisting the construction of an avionics platform according to claim 10, wherein the functional description includes a list of the avionics functions and of the links between them, a list of the software modules enabling the avionics functions to be executed, and of the functional link occurrences between these software modules, and the material description includes a list of calculation or communication items of equipment, as well as a list of the physical links between the calculation or communication items of equipment.

5. A method for assisting the construction of an avionics platform, using a tool including:

a first functional database in which is stored a functional description of the said platform,

a second material database in which is stored a material description of the said platform, and

a workstation, linked to the first and second databases,

wherein said method is to implement a set of avionics functions, where each avionics function comprises one or more software modules, and where any two software modules can exchange messages based on a link, known as a functional link occurrence, and

wherein said avionics platform includes;

items of equipment linked together by unidirectional or bidirectional physical links belonging to different types of networks, and

paths enabling linking of said equipment, where each path consists of one of the following;

a single direct physical link between a source item of equipment and a destination item of equipment,

a first physical link between said source item of equipment and a first network node,

a second physical link between said destination item of equipment and a second network node, and

at least a third physical link between said first and second nodes, the method comprising;

associating each software module with an item of equipment onto which said software module is intended to be hosted;

for each functional link occurrence, providing to the workstation a list of all possible topological paths enabling a first item of equipment and a second item of equipment respectively hosting corresponding software modules to be linked;

receiving from the workstation a selection of one of the topological paths from the list;

associating each functional link occurrence with a corresponding selected topological path to let pass through each functional link occurrence the messages of the functional link occurrence;

checking each equipment as to whether each item of equipment has sufficient material resources to allow execution of the software module or modules which is/are associated with each item of equipment;

listing in a source list for each source item of equipment the types of physical links associated with the connection resources of the connectors of each source item of equipment,

selecting a type of link from among the types of links listed in each source list;

listing in a receiving list the items of equipment having connection resources capable of receiving the type of link thus selected; and

selecting a destination item of equipment from among the items of equipment listed in each receiving list.

6. The method for assisting the construction of an avionics platform according to claim 5, further comprising:

generating a path between the source item of equipment and the destination item of equipment by creating a new physical link of said selected type of link between these two items of equipment, if the latter is of the first or third type, the generated path being then associated with the physical link created in this fashion, and being unidirectional in the case of the first type and bidirectional in the case of the third type.

7. The method for assisting the construction of an avionics platform according to claim 5, further comprising:

generating a path between the source item of equipment and the destination item of equipment by associating it with an existing physical link or by creating a new link of said selected type between these two items of equipment, if said selected type is of the second or fourth type, the generated path being then associated with the existing or created link, and being unidirectional in the case of the second type and bidirectional in the case of the fourth type.

8. The method for assisting the construction of an avionics platform according to claim 6 or 7, further comprising:

checking as to whether the connection resources of the connectors of the source item of equipment, on the one hand, and those of the connectors of the destination item of equipment, on the other, are sufficient to receive the new created physical links;

validating the generated path if the connection resources are sufficient; and

invalidating the generated path if the connection resources are not sufficient.