Managing flight paths of a soaring aircraft with crowd sourcing
Disclosed is a novel system and method for adjusting a flight path of an aircraft. The method begins with computing a flight path of an aircraft from a starting point to an ending point which incorporates predicted weather effects at different points in space and time. An iterative loop is entered for the flight path. Each of the following steps are performed in the iterative loop. First lift data is accessed from a fine-grain weather model associated with a geographic region of interest. The lift data is data to calculate a force that directly opposes a weight of the aircraft. In addition, lift data is accessed from sensors coupled to the aircraft. The lift data is one or more of 1) thermal data, 2) ridge lift data, 3) wave lift data, 3) convergence lift data, and 4) a dynamic soaring lift data. Numerous embodiments are disclosed.
1. A computer-implemented method for adjusting a flight path of an aircraft, the method comprising:
computing a flight path of an aircraft from a starting point to an ending point which incorporates predicted weather effects at different points in space and time;
during a flight path performing each of:
accessing lift data from a fine-grained weather model associated with a geographic region of interest, the lift data being data to calculate a force that directly opposes a weight of the aircraft, and the fine-grained weather model providing weather to the geographic region of interest being less than a kilometer with a type of lift from categories of a ridge lift, a wave lift, and a dynamic soaring lift along with a time period in minutes in which the lift data for the type of lift is applicable;
accessing lift data from sensors on the aircraft;
accessing lift data from a group of people that elect to share data for a specific flight path;
computing adjustments to the flight path based on a combination of the lift data from the fine-grain weather model, the lift data from sensors and the lift data from the group of people; and
adjusting the flight path using the adjustments that have been computed.
2. The computer-implemented method of claim 1 , further comprising:
sending the flight path as it is adjusted to a second aircraft.
3. The computer-implemented method of claim 2 , further comprising:
receiving adjustments to the flight path from the second aircraft in order to avoid collisions therewith.
4. The computer-implemented method of claim 1 , further comprising:
receiving, on a second aircraft, lift data from sensors coupled to the aircraft; and
computing adjustments to the flight path of the aircraft is performed on a second aircraft; and
receiving from the second aircraft the adjustments which have been computed on the second aircraft.
5. The computer-implemented method of claim 1 , further comprising:
receiving, on a second aircraft, lift data from sensors coupled to the aircraft; and
wherein at least a portion of the computing adjustments to the flight path of the aircraft is performed by both the aircraft and the second aircraft.
6. The computer-implemented method of claim 1 , wherein the aircraft is unpowered.
7. The computer-implemented method of claim 1 , wherein the aircraft is powered by one or more engines.
8. The computer-implemented method of claim 1 , wherein at least one of
computing a flight path of an aircraft from the starting point to the ending point, and
adjusting the flight path using the adjustments that have been computed, includes using a portion of the flight path that has been previously computed to rank a reliability of the portion of the flight path.
9. An aircraft flight path processor system comprising:
a memory;
a processor communicatively coupled to the memory, where the processor is configured to perform
computing a flight path of an aircraft from a starting point to an ending point which incorporates predicted weather effects at different points in space and time;
during a flight path performing each of:
accessing lift data from a fine-grained weather model associated with a geographic region of interest, the lift data being data to calculate a force that directly opposes a weight of the aircraft, and the fine-grained weather model providing weather to the geographic region of interest being less than a kilometer with a type of lift from categories of a ridge lift, a wave lift, and a dynamic soaring lift along with a time period in minutes in which the lift data for the type of lift is applicable;
accessing lift data from sensors on the aircraft;
accessing lift data from a group of people that elect to share data for a specific flight path;
computing adjustments to the flight path based on a combination of the lift data from the fine-grain weather model, the lift data from sensors and the lift data from the group of people; and
adjusting the flight path using the adjustments that have been computed.
10. The aircraft flight path processor system of claim 9 , further comprising: sending the flight path as it is adjusted to a second aircraft.
11. The aircraft flight path processor system of claim 10 , further comprising: receiving adjustments to the flight path from the second aircraft in order to avoid collisions therewith.
12. The aircraft flight path processor system of claim 9 , further comprising:
receiving, on a second aircraft, lift data from sensors coupled to the aircraft; and
computing adjustments to the flight path of the aircraft is performed on a second aircraft; and
receiving from the second aircraft the adjustments which have been computed on the second aircraft.
13. The aircraft flight path processor system of claim 9 , further comprising:
receiving, on a second aircraft, lift data from sensors coupled to the aircraft; and
wherein at least a portion of the computing adjustments to the flight path of the aircraft is performed by both the aircraft and the second aircraft.
14. The aircraft flight path processor system of claim 9 , wherein the aircraft is unpowered.
15. The aircraft flight path processor system of claim 9 , wherein the aircraft is powered by one or more engines.
16. The aircraft flight path processor system of claim 9 , wherein at least one of
computing a flight path of an aircraft from the starting point to the ending point, and
adjusting the flight path using the adjustments that have been computed, includes using a portion of the flight path that has been previously computed to rank a reliability of the portion of the flight path.
17. A non-transitory computer program product for adjusting flight path of an aircraft, the non-transitory computer program product comprising a computer readable storage medium having program code embodied therewith, the program code executable on processor to perform:
computing a flight path of an aircraft from a starting point to an ending point which incorporates predicted weather effects at different points in space and time;
during a flight path performing each of:
accessing lift data from a fine-grained weather model associated with a geographic region of interest, the lift data being data to calculate a force that directly opposes a weight of the aircraft, and the fine-grained weather model providing weather to the geographic region of interest being less than a kilometer with a type of lift from categories of a ridge lift, a wave lift, and a dynamic soaring lift along with a time period in minutes in which the lift data for the type of lift is applicable;
accessing lift data from sensors on the aircraft;
accessing lift data from a group of people that elect to share data for a specific flight path;
computing adjustments to the flight path based on a combination of the lift data from the fine-grain weather model, the lift data from sensors and the lift data from the group of people; and
adjusting the flight path using the adjustments that have been computed.