Systems and methods for representation of a flight vehicle in a controlled environment
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
G06F-019/00
G05D-001/00
출원번호
US-0304229
(2005-12-14)
등록번호
US-7457690
(2008-11-25)
발명자
/ 주소
Wilson, Jr.,Robert C.
Whitley,Ted D.
Estkowski,Regina
출원인 / 주소
Wilson, Jr.,Robert C.
Whitley,Ted D.
Estkowski,Regina
인용정보
피인용 횟수 :
21인용 특허 :
11
초록▼
Systems and methods for representing a flight vehicle in a controlled environment are disclosed. In one embodiment, a system comprises a communications link that extends between a ground-based facility and at least one flight vehicle operating within the controlled environment that is operable to co
Systems and methods for representing a flight vehicle in a controlled environment are disclosed. In one embodiment, a system comprises a communications link that extends between a ground-based facility and at least one flight vehicle operating within the controlled environment that is operable to communicate trajectory data between the ground-based facility and the at least one flight vehicle, and a processor configured to generate the trajectory data.
대표청구항▼
What is claimed is: 1. A system for representing a flight vehicle in a controlled environment, comprising: means for generating trajectory data for the flight vehicle, the trajectory data including predicted trajectory of the vehicle; and means for communicating the trajectory data between a receiv
What is claimed is: 1. A system for representing a flight vehicle in a controlled environment, comprising: means for generating trajectory data for the flight vehicle, the trajectory data including predicted trajectory of the vehicle; and means for communicating the trajectory data between a receiving facility and the flight vehicle; wherein the predicted trajectory is used to increase reliability of at least one of data communications and commanded trajectory of the vehicle during flight. 2. The system of claim 1, wherein the trajectory data further includes a commanded trajectory. 3. The system of claim 2, wherein the means for generating the trajectory data includes a processor for processing an actual trajectory matrix, a command trajectory matrix and a predicted trajectory matrix, and for comparing the command trajectory matrix with the predicted trajectory matrix and altering the command trajectory matrix based upon the comparison. 4. The system of claim 1, wherein the receiving facility includes at least one of an air-route traffic control center (ARTCC), a terminal radar approach control facility (TRACON), a flight service station (FSS) and a control tower. 5. The system of claim 1, wherein the actual trajectory includes at least one of an actual positional vector, an actual rate vector, an aircraft identification vector, an aircraft attitude vector and a frequency vector. 6. The system of claim 2, wherein the commanded trajectory includes at least one of a command positional vector, a command rate vector, a command deviation vector and a command frequency vector. 7. The system of claim 1, wherein the predicted trajectory includes at least one of a predicted spacing vector and an altitude vector. 8. The system of claim 1, wherein the means for generating the trajectory data includes at least one processor that is positioned in at least one of the ground-based facility and the flight vehicle. 9. The system of claim 1, wherein the means for communicating the trajectory data includes equipment for communicating via at least one of a communications satellite and an aerostat, the equipment operable to relay the trajectory data between the ground-based facility and the flight vehicle. 10. The system of claim 1, wherein the means for communicating the trajectory data includes an aircraft communications and reporting system (ACARS). 11. The method of claim 1, wherein the actual and predicted trajectories are determined on-board the flight vehicle and sent to the ground facility. 12. A method of representing a flight vehicle in a controlled environment, comprising: generating an actual trajectory for the flight vehicle and communicating the actual trajectory to a receiving facility; compiling a command trajectory that conforms to a desired course and altitude for the flight vehicle and a predicted trajectory that includes at least a minimum spacing between flight vehicles within the controlled environment; communicating the command trajectory to the flight vehicle; comparing the command trajectory to the predicted trajectory to determine if a conflict exists; and if a conflict exists, altering the command trajectory to remove the conflict. 13. The method of claim 12, wherein generating an actual trajectory further comprises generating an actual trajectory matrix that includes at least one of an actual positional vector, an actual rate vector, an aircraft identification vector, an aircraft attitude vector and a frequency vector. 14. The method of claim 12, wherein compiling a command trajectory further comprises compiling a command trajectory matrix that includes at least one of a command positional vector, a command rate vector, a command deviation vector and a command frequency vector. 15. The method of claim 12, wherein compiling a predicted trajectory further comprises compiling a predicted trajectory matrix that includes at least one of a predicted spacing vector and an altitude vector. 16. The method of claim 12, wherein the predicted trajectory is a function of an actual trajectory from at least one other flight vehicle. 17. The method of claim 12, wherein communicating the command trajectory to the flight vehicle further comprises communicating the command trajectory between a ground-based facility and the flight vehicle. 18. A system for managing a plurality of flight vehicles in a controlled airspace environment, comprising: a ground-based facility operable to receive actual trajectory data from each of the flight vehicles and generate command trajectory data for each of the flight vehicles, the facility communicating the command trajectory data to the vehicles, predicted trajectory data also being communicated between the facility and the vehicles, the communicated data used to enhance reliability of at least one of data communications and commanded trajectory of the vehicles during flight. 19. The system of claim 18, wherein the actual and predicted trajectory data is used to increase reliability with respect to communicatons latency. 20. The system of claim 18, wherein the actual and predicted trajectory data is used to increase reliability with respect to aircraft control and safety.
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이 특허에 인용된 특허 (11)
Vaida, Theodore F.; McKenna, Andrew M., Aircraft location monitoring system and method of operation.
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Casado Magaña, Enrique Juan; D'Alto, Luis Pedro; Vilaplana Ruiz, Miguel, Determining a descent trajectory described by an aircraft intent description language (AIDL).
Breen, Thomas J.; Smith, Alexander E.; Rossano, Christopher F., Extension of aircraft tracking and positive identification from movement areas into non-movement areas.
Smith, Alexander E.; Hulstrom, Russell; Evers, Carl A.; Breen, Thomas J., Method and apparatus for ADS-B validation, active and passive multilateration, and elliptical surviellance.
Castillo-Effen, Mauricio; Chan, David So Keung; Tomlinson, Jr., Harold Woodruff; Klooster, Joel Kenneth; Torres, Sergio, Methods and systems for inferring aircraft parameters.
Subbu, Rajesh Venkat; Xue, Feng; Castillo-Effen, Mauricio; Klooster, Joel Kenneth; Hochwarth, Joachim Karl; Torres, Sergio; Chen, Weiwei, Methods and systems for managing air traffic.
Subbu, Rajesh Venkat; Xue, Feng; Castillo-Effen, Mauricio; Klooster, Joel Kenneth; Hochwarth, Joachim Karl; Torres, Sergio; Chen, Weiwei, Methods and systems for managing air traffic.
Subbu, Rajesh Venkat; Chan, David So Keung; Brooksby, Glen William; Klooster, Joel Kenneth; Torres, Sergio, Schedule management system and method for managing air traffic.
Estkowski, Regina I.; Whitley, Ted Dell; Baumeister, Richard; Spence, Graham, System and methods for situation awareness, advisory, tracking, and aircraft control information.
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