Method of controlling an aircraft, the method implementing a vote system
In the method of controlling an aircraft, a device implements the steps consisting in determining a first global value on the basis of only some amongst first individual values calculated by respective applications, modifying at least one parameter to take account of how the determination step took place and determining a second global value on the basis of second individual values calculated by the respective applications and on the basis of the parameter(s).
1. A method of controlling an aircraft, comprising:
determining a first global value on the basis of more than one, but not all, first individual values, each of the first individual values calculated by its respective applications; then
analyzing results of the determining of the first global value; then
modifying at least one parameter to take account of how the determination step took place; and then
determining a second global value on the basis of second individual values, each of the second individual values calculated by its respective applications, and additionally on the basis of the at least one parameter,
wherein a device implements the determining a first global value, analyzing, modifying, and determining a second global value steps.
2. A method according to claim 1 , wherein the first global value is identical to a majority of the first individual values.
3. A method according to claim 2 wherein the majority is an absolute majority.
4. A method according to claim 1 , wherein the first determination step is implemented without taking account of the at least one parameter.
5. A method according to claim 1 , wherein the at least one parameter is a weighting coefficient allocated to one of the respective applications.
6. A method according to claim 1 , wherein, during the modification step, the device modifies the at least one parameter associated with one of the respective applications that calculated a first individual value that was different from the first global value.
7. A method according to claim 6 wherein during the modification step the device leaves at least one other parameter unchanged.
8. A method according to claim 1 , wherein, during the second determination step, the second individual values are such that either they are two in number and different from each other, or else they are distributed in value groups, the values in any one group being mutually identical and different from those in the other groups, the groups having the highest cardinal number being at least two in number and having the same cardinal number.
9. A computer program embodied on a non-transitory computer readable medium for controlling the implementation of a method when executed on a computer, the method comprising:
determining a first global value on the basis of more than one, but not all, first individual values, each of the first individual values calculated by its respective applications; then
analyzing results of the determining of the first global value; then
modifying at least one parameter to take account of how the determination step took place; and then
determining a second global value on the basis of second individual values, each of the second individual values calculated by its respective applications, and additionally on the basis of the at least one parameter,
wherein a device implements the determining a first global value, analyzing, modifying, and determining a second global value steps.
10. A device for controlling an aircraft, wherein the device comprises:
determining a first global value on the basis of more than one, but not all, first individual values, each of the first individual values calculated by its respective applications;
analyzing results of the determined first global value;
modifying at least one parameter to take account of the way in which the determination step took place; and
determining a second global value on the basis of second individual values, each of the second individual values calculated by its respective applications and additionally on the basis of the at least one parameter.
11. A system for controlling an aircraft, the system comprising a device and applications for providing individual values to the device, wherein the device comprises:
determining a first global value on the basis of more than one, but not all, first individual values, each of the first individual values calculated by its respective applications;
analyzing results of the determined first global value;
modifying at least one parameter to take account of the way in which the determination step took place; and
determining a second global value on the basis of second individual values, each of the second individual values calculated by its respective applications and additionally on the basis of the at least one parameter.
12. A system according to claim 11 wherein the number of applications is even.
13. An aircraft including a device for controlling an aircraft, wherein the device comprises:
determining a first global value on the basis of only more than one, but not all, first individual values, each of the first individual values calculated by its respective applications;
analyzing results of the determining of the first global value;
modifying at least one parameter to take account of the way in which the determination step took place; and
determining a second global value on the basis of second individual values, each of the second individual values calculated by its respective applications and additionally on the basis of the at least one parameter.