Risk-based flight path data generating system, device, and method
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
G08G-005/00
G05D-001/00
G05D-001/10
출원번호
US-0814760
(2015-07-31)
등록번호
US-9542849
(2017-01-10)
발명자
/ 주소
Bertram, Joshua R.
Vogl, Thomas L.
Wolford, Brian R.
출원인 / 주소
Rockwell Collins, Inc.
대리인 / 주소
Barbieri, Daniel M.
인용정보
피인용 횟수 :
3인용 특허 :
13
초록▼
A system, device, and method for generating and employing risk-based flight path data are disclosed. The system for employing risk-based flight path data may include one or more one avionics systems and/or remote aircraft operator systems configured to receive risk-based flight path data from a rout
A system, device, and method for generating and employing risk-based flight path data are disclosed. The system for employing risk-based flight path data may include one or more one avionics systems and/or remote aircraft operator systems configured to receive risk-based flight path data from a route generator (RG). The RG may acquire navigation data representative of one or more waypoints, acquire risk object data based upon the navigation data, determine the risk-based flight path data representative of a risk-based flight path as a function of the acquired navigation data, the acquired risk data, and a route generating algorithm, and provide the flight path data to the one or more avionics systems and/or remote aircraft operator systems. In some embodiments, the risk object data may include a plurality of risk clearance altitudes. In other embodiments, the risk object data may include a plurality of risk clearance elevations.
대표청구항▼
1. A system for generating risk-based flight path data, comprising: at least one of an avionics system and a remote aircraft operator system configured to: receive risk-based flight path data provided by a path generator including at least one processor coupled to a non-transitory processor-readable
1. A system for generating risk-based flight path data, comprising: at least one of an avionics system and a remote aircraft operator system configured to: receive risk-based flight path data provided by a path generator including at least one processor coupled to a non-transitory processor-readable medium storing processor-executable code and configured to: acquire navigation data representative of a plurality of waypoints;acquire risk-based, elevation data based upon the navigation data and comprised of first data representative of a plurality of risk elevations of a plurality of elevation cells of a digital risk model of elevations, or second data determinative of a plurality of risk elevations of a plurality of elevation cells of a digital risk model of elevations, where a value for each of the risk elevations of the first data or the second data is based upon a plurality of surface elevations of a plurality of surface elevation cells of a digital elevation model adjusted for a level of risk of a crash of an aircraft and a cost corresponding to harm or injury to at least one person, at least one object on the ground, or both arising from the crash;determine a risk-based flight path for the aircraft based upon the acquired navigation data, the acquired risk-based, elevation data, and a route generating algorithm;generate flight path data representative of the risk-based flight path; andprovide the flight path data to at least one of an avionics system and a remote aircraft operator system, wherein a first avionics system comprised of at least one system of an autoflight system of the aircraft is configured to receive and employ the flight path data, a second avionics system comprised of a display system of the aircraft is configured to receive the flight path data and present risk-based flight path information to a viewer located inside the aircraft, or the remote aircraft operator system is configured to receive the flight path data and present risk-based flight path information to a viewer located outside the aircraft. 2. The system of claim 1, wherein the second data is comprised of the plurality of surface elevations of the plurality of surface elevation cells of the digital elevation model, anda plurality of risk clearance altitudes of a plurality of risk clearance altitude cells of a digital risk model of clearance altitudes. 3. The system of claim 2, wherein at least a portion of the plurality of risk clearance altitudes is based upon a probability curve of a probability distribution function applied to the portion of the plurality of risk clearance altitudes. 4. The system of claim 2, wherein at least a portion of the plurality of risk elevations is based upon a probability curve of a probability distribution function applied to the portion of the plurality of risk elevations. 5. The system of claim 1, wherein the risk-based, elevation data is further comprised of third data representative of a plurality of risk ceilings of a plurality of risk ceiling cells of a digital risk model of ceilings. 6. A device for generating risk-based flight path data, comprising: a path generator including at least one processor coupled to a non-transitory processor-readable medium storing processor-executable code and configured to: acquire navigation data representative of a plurality of waypoints;acquire risk-based, elevation data based upon the navigation data and comprised of first data representative of a plurality of risk elevations of a plurality of elevation cells of a digital risk model of elevations, orsecond data determinative of a plurality of risk elevations of a plurality of elevation cells of a digital risk model of elevations, where a value for each of the risk elevations of the first data or the second data is based upon a plurality of surface elevations of a plurality of surface elevation cells of a digital elevation model adjusted for a level of risk of a crash of an aircraft and a cost corresponding to harm or injury to at least one person, at least one object on the ground, or both arising from the crash;determine a risk-based flight path for the aircraft based upon the acquired navigation data, the acquired risk-based, elevation data, and a route generating algorithm;generate flight path data representative of the risk-based flight path; andprovide the flight path data to at least one of an avionics system and a remote aircraft operator system, wherein a first avionics system comprised of at least one system of an autoflight system of the aircraft is configured to receive and employ the flight path data,a second avionics system comprised of a display system of the aircraft is configured to receive the flight path data and present risk-based flight path information to a viewer located inside the aircraft, ora remote aircraft operator system is configured to receive the flight path data and present risk-based flight path information to a viewer located outside the aircraft. 7. The device of claim 6, wherein the second data is comprised of the plurality of surface elevations of the plurality of surface elevation cells of the digital elevation model, anda plurality of risk clearance altitudes of a plurality of risk clearance altitude cells of a digital risk model of clearance altitudes. 8. The device of claim 7, wherein at least a portion of the plurality of risk clearance altitudes is based upon a probability curve of a probability distribution function applied to the portion of the plurality of risk clearance altitudes. 9. The device of claim 7, wherein at least a portion of the plurality of risk elevations is based upon a probability curve of a probability distribution function applied to the portion of the plurality of risk elevations. 10. The device of claim 6, wherein the risk-based, elevation data is further comprised of third data representative of a plurality of risk ceilings of a plurality of risk ceiling cells of a digital risk model of ceilings. 11. A method for generating risk-based flight path data, comprising: acquiring, by a path generator including at least one processor coupled to a non-transitory processor-readable medium storing processor-executable code, navigation data representative of a plurality of waypoints;acquiring risk-based, elevation data based upon the navigation data and comprised of first data representative of a plurality of risk elevations of a plurality of elevation cells of a digital risk model of elevations, orsecond data determinative of a plurality of risk elevations of a plurality of elevation cells of a digital risk model of elevations, where a value for each of the risk elevations of the first data or the second data is based upon a plurality of surface elevations of a plurality of surface elevation cells of a digital elevation model adjusted for a level of risk of a crash of an aircraft and a cost corresponding to harm or injury to at least one person, at least one object on the ground, or both arising from the crash;determining a risk-based flight path for the aircraft based upon the acquired navigation data, the acquired risk-based, elevation data, and a route generating algorithm;generating flight path data representative of the risk-based flight path; andproviding the flight path data to at least one of an avionics system and a remote aircraft operator system, wherein a first avionics system comprised of at least one system of an autoflight system of the aircraft is configured to receive and employ the flight path data,a second avionics system comprised of a display system of the aircraft is configured to receive the flight path data and present risk-based flight path information to a viewer located inside the aircraft, ora remote aircraft operator system is configured to receive the flight path data and present risk-based flight path information to a viewer located outside the aircraft. 12. The method of claim 11, wherein the second data is comprised of the plurality of surface elevations of the plurality of surface elevation cells of the digital elevation model, anda plurality of risk clearance altitudes of a plurality of risk clearance altitude cells of a digital risk model of clearance altitudes. 13. The method of claim 12, wherein at least a portion of the plurality of risk clearance altitudes is based upon a probability curve of a probability distribution function applied to the portion of the plurality of risk clearance altitudes. 14. The method of claim 12, further comprising: acquiring aircraft performance data representative of an availability or unavailability of at least one aircraft system configured with at least at least one input factor from which real-time aircraft performance is determined, such that the plurality of risk clearance altitudes is modified, where the modification is based upon the availability or unavailability of the at least one aircraft system. 15. The method of claim 12, wherein at least a portion of the plurality of risk elevations is based upon a probability curve of a probability distribution function applied to the portion of the plurality of risk elevations. 16. The method of claim 12, further comprising: acquiring aircraft performance data representative of an availability or unavailability of at least one aircraft system configured with at least at least one input factor from which real-time aircraft performance is determined, such that the plurality of risk elevations is modified, where the modification is based upon the availability or unavailability of the at least one aircraft system. 17. The method of claim 11, wherein the risk-based, elevation data is further comprised of third data representative of a plurality of risk ceilings of a plurality of risk ceiling cells of a digital risk model of ceilings. 18. The method of claim 17, wherein at least a portion of the plurality of risk ceilings is based upon a probability curve of a probability distribution function applied to the portion of the plurality of risk ceilings. 19. The method of claim 17, further comprising: acquiring aircraft performance data representative of an availability or unavailability of at least one aircraft system configured with at least at least one input factor from which real-time aircraft performance is determined, such thatthe plurality of risk ceilings is modified, where the modification is based upon the availability or unavailability of the at least one aircraft system. 20. The method of claim 11, further comprising: acquiring aircraft performance data representative of an availability or unavailability of at least one aircraft system configured with at least at least one input factor from which real-time aircraft performance is determined, such that the basis for determining the risk-based flight path includes the aircraft performance data.
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이 특허에 인용된 특허 (13)
Vaida, Theodore F., Aircraft flight risk measuring system and method of operation.
Bacabara, Corinne; Nouvel, Christian, Display device for an aircraft including means for displaying a navigation symbology dedicated to obstacle avoidance.
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