초록 ▼

The invention concerns a method and a system for calculating a flight route between a first position and a second position. According to the method, the first position is chosen as the current position, and the following steps are then repeated until the second position is reached: a loss function i

The invention concerns a method and a system for calculating a flight route between a first position and a second position. According to the method, the first position is chosen as the current position, and the following steps are then repeated until the second position is reached: a loss function is determined corresponding to each flight path in a set of flight paths that are predefined in relation to the current direction of flight; a flight path that yields the most advantageous value for the loss function is selected; a subsection from the current position and a predetermined number of positions forward are registered for the selected flight path, and the position at the end of the subsection is chosen as the new current position.

대표청구항 ▼

The invention claimed is: 1. A method for calculating a flight route between a first position and a second position, wherein the first position is initially chosen as a current position, and wherein the following steps are repeated until the second position is reached: a loss function is determined

The invention claimed is: 1. A method for calculating a flight route between a first position and a second position, wherein the first position is initially chosen as a current position, and wherein the following steps are repeated until the second position is reached: a loss function is determined corresponding to each flight path in a set of flight paths that are predefined in relation to a current direction of flight; a flight path that yields a most advantageous value for the loss function is selected; a subsection from the current position and a predetermined number of positions forward are registered for the selected flight path; a position at an end of the subsection is chosen as a new current position; wherein after the flight route has been calculated between the first and the second position, the calculated route is refined in a refining step, in which registered points that are located as far from one another as possible but between which unobstructed visibility prevails are marked as breakpoints, and in that the route is chosen as straight lines between these marked breakpoints. 2. A method according to claim 1, wherein the loss function includes at least a subset of the following parameters: a first parameter that indicates whether the selected flight path crosses predefined threat zones; a second parameter that indicates whether the selected flight path passes too near to terrain; a third parameter that indicates whether the selected flight path exceeds a predefined altitude value; a fourth parameter that indicates whether the selected flight path is costly from a fuel standpoint; a fifth parameter that indicates a distance to a second position of the route. 3. A method according to claim 1, wherein the flight paths in the flight path set are selected based on a control signal sequence belonging to each flight path. 4. A method according to claim 3, wherein a second through a final signal in each control signal sequence are zeroed. 5. A method according to claim 1, wherein the predetermined number of positions forward is one. 6. A system for calculating a flight route for an aircraft between a first position and a second position, wherein the system comprises: a terrain database arranged so as to store terrain data, including latitude and longitude data with associated altitude data; a threat database arranged so as to store data concerning threats, including at least data concerning a geographical extent of the threats; a first calculating unit that is operatively connected to the terrain database and the threat database and arranged so as to calculate a route between the first and the second positions, whereupon the first calculating unit operates according to a predetermined scheme, wherein the first position is initially selected as a current position, and wherein the following steps are repeated until the second position is reached: a loss function is determined corresponding to each flight path in a set of flight paths that are predefined in relation to a current direction of flight; a flight path that yields a most advantageous value for the loss function is selected; a subsection from the current position and a predetermined number of positions forward are registered for the selected flight path, and a position at an end of the subsection is chosen as a new current position; and wherein the first calculating unit, the terrain database and the threat database are operatively connected to a second calculating unit, which is arranged so as to receive the flight route calculated by the first calculating unit and refine it, whereupon registered points that are located as far as possible from one another, but between which unobstructed visibility prevails, are marked as breakpoints, and in that the route is chosen as straight lines between these marked breakpoints. 7. A system according to claim 6, characterized in that the entire system is implemented in the aircraft. 8. A system according to claim 6, characterized in that the system is partly implemented in the aircraft and partly in a ground-based station, whereupon data are communicated between the aircraft the ground-based station via a link.