Configurable communication systems and methods for communication
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
H04L-029/08
H04B-001/3822
H04B-007/26
H04L-012/725
출원번호
US-0172406
(2014-02-04)
등록번호
US-9826039
(2017-11-21)
발명자
/ 주소
Goldstein, David B.
Frost, Wendell
출원인 / 주소
HONEYWELL INTERNATIONAL INC.
대리인 / 주소
Lorenz & Kopf, LLP
인용정보
피인용 횟수 :
0인용 특허 :
124
초록▼
A method is provided for managing communications from a computing device of a vehicle. The method includes receiving configuration parameters generated by a user; determining a communication priority scheme based on the configuration parameters; communicating a first subset of data according to a fi
A method is provided for managing communications from a computing device of a vehicle. The method includes receiving configuration parameters generated by a user; determining a communication priority scheme based on the configuration parameters; communicating a first subset of data according to a first communication medium based on the communication priority scheme; and communicating a second subset of data according to a second communication medium based on the communication priority scheme.
대표청구항▼
1. A method for managing communications from a computing device of a vehicle wherein the computing device is located within the vehicle for managing the communications to ground elements, the computing device comprising: receiving, by a parameter module, configuration parameters entered by a user th
1. A method for managing communications from a computing device of a vehicle wherein the computing device is located within the vehicle for managing the communications to ground elements, the computing device comprising: receiving, by a parameter module, configuration parameters entered by a user through a user interface, the configuration parameters comprising a plurality of attributes of a communication medium, the attributes comprising cost, speed, reliability, data criticality, and communication path in use wherein the vehicle is an aircraft and the user interface is located within a cockpit of the aircraft or alternatively at other locations within the aircraft;determining, by a priority module coupled to the parameter module, a communication priority scheme for a plurality of conditions of the ground elements based on the configuration parameters wherein the plurality attributes of the configuration parameters comprise a ranking accordingly for a particular condition;evaluating by a communication determination module the communication priority scheme by one or more attributes of the plurality of attributes related to the priority scheme with available communication mediums for a communication path through one or more of the available communication mediums for transmission of data to the ground elements wherein the one or more attributes at least comprise: priority for a lowest cost or a highest reliability for the transmission of the data;communicating, by a communication module based on an evaluation from the communication determination module, to the ground elements a first subset of data for transmission according to a first communication medium with the communication priority scheme associated therewith;responding during the transmission of the first subset of data to a change in the communication mediums to the ground elements comprising an update in the communication path from a current communication medium to another communication medium whereby an available communication management module pauses an ongoing transmission on the first communication medium, switches the ongoing transmission to an alternative communication path with the available communication mediums and resumes the ongoing transmissions on the alternative communication path wherein the current communication medium is the first communication medium with the associated communication priority scheme; andcommunicating, subsequently upon a completion of the transmission of the first subset of data, to the ground elements a second subset of data according to a second communication medium based on the communication priority scheme. 2. The method of claim 1, wherein the receiving the configuration parameters is based on a stored configuration file. 3. The method of claim 1, wherein the configuration parameters further comprise a ranking of the attributes of a communication medium. 4. The method of claim 1, wherein the configuration parameters further comprise at least one condition associated with at least one of rankings of the attributes and the attributes. 5. The method of claim 4, wherein the at least one condition is further associated with at least one of security of data to be transmitted, criticality of data to be transmitted, and an operational state of the vehicle. 6. The method of claim 1, wherein the communicating the first subset of data is further based on attributes of the available communication mediums. 7. A communication system for a computing device wherein the computing device is located within a vehicle for managing the communications to ground elements, comprising: a non-transitory computer readable medium comprising: a parameter module,that receives configuration parameters entered by a user through a user interface, the configuration parameters comprising attributes of a communication medium, the attributes comprising cost, speed, reliability, data criticality, and communication path in use wherein the vehicle is an aircraft and the user interface is located within a cockpit of the aircraft or alternatively at other locations within the aircraft;a priority module coupled to the parameter module, that determines a communication priority scheme based on the configuration parameters for a plurality of conditions of the ground elements;a communication determination module that evaluates the communication priority scheme with available communication mediums for a communication path through one or more of the available communication mediums for transmission of data to the ground elements;a communication module that communicates based on an evaluation from the communication determination module, to the ground elements a first subset of data for transmission according to a first communication medium with the communication priority scheme associated therewith,that responds during the transmission of the first subset of data to a change in the communication mediums to the ground elements which comprises an update in the communication path from a current communication medium to another communication medium whereby an available communication management module pauses an ongoing transmission on the first communication medium, switches the ongoing transmission to an alternative communication path with the available communication mediums and resumes the ongoing transmissions on the alternative communication path wherein the current communication medium is the first communication medium with the associated communication priority scheme;andthat communicates, subsequently upon a completion of the transmission of the first subset of data, to the ground elements a second subset of data according to a second communication medium based on the communication priority scheme. 8. The communication system of claim 7, wherein the parameter module receives the configuration parameters based on a stored configuration file. 9. The communication system of claim 7, wherein the configuration parameters comprise a ranking of the attributes of a communication medium. 10. The communication system of claim 7, wherein the configuration parameters comprise at least one condition associated with at least one of the rankings of attributes and the attributes. 11. The communication system of claim 10, wherein the at least one condition is associated with at least one of security of data to be transmitted, criticality of data to be transmitted, and an operational state of an aircraft. 12. A computing device of an aircraft, comprising: a non-transitory computer readable medium wherein the computing device is located within the aircraft for managing the communications to ground elements, comprising: a parameter module,that receives configuration parameters entered by a user through a user interface, the configuration parameters comprising attributes of a communication medium, the attributes comprising cost, speed, reliability, data criticality, and communication path in use wherein the user interface is located within a cockpit of the aircraft or alternatively at other locations within the aircraft;a priority module coupled to the parameter module, that determines a communication priority scheme based on the configuration parameters for a plurality of conditions of the ground elements;a communication determination module that evaluates the communication priority scheme with available communication mediums for a communication path through one or more of the available communication mediums for transmission of data to the ground elements;a communication module that communicates based on an evaluation from the communication determination module, to the ground elements a first subset of data for transmission according to a first communication medium with the communication priority scheme associated therewith; andthat communicates a second subset of data according to a second communication medium based on the communication priority scheme to the ground elements.
연구과제 타임라인
LOADING...
LOADING...
LOADING...
LOADING...
LOADING...
이 특허에 인용된 특허 (124)
Bantoft, Ken; Gray, Curt, Air to ground management of multiple communication paths.
Ziarno,James J.; Gallagher,Shawn, Aircraft communications system and related method for communicating between portable wireless communications device and ground.
Eicke, Michael Dennis; Hostetler, Jeffrey K.; Griffin, Edward M.; Cawood, Michael D., Apparatus, program product, and methods for updating data on embedded control systems.
Wakumoto, Shaun Kazuo; Bare, Ballard Claude; Ersoy, Cetin, Determination of a plurality of paths before selection of one path of the plurality of paths for transmission of one or more packets.
Archer, Charles J.; Blocksome, Michael A.; Smith, Brian E., Dynamic network link selection for transmitting a message between compute nodes of a parallel computer.
D'Errico, Matthew J., Method and apparatus for balancing workloads among paths in a multi-path computer system based on the state of previous I/O operations.
Urban, Jeffrey; Barhorst, Jeffrey; Solomon, Christopher C.; Edwards, Herbert; Oltrogge, Chris; Albert, Adam, Method and apparatus for transportation of data over a managed wireless network using unique communication protocol.
Holst, William; Lee, David Richard, Method and apparatus to support remote and automatically initiated data loading and data acquisition of airborne computers using a wireless spread spectrum aircraft data services link.
Brady, Jr., Kenneth A.; Yi, Jason Kyong-min; Weimholt, Andrew W.; Tsaur, Jyh-Fong; Norton, Lyle K., Method and system for configuration and download in a restricted architecture network.
Korson,Shannon Lee; Garls,Sharon Ann; Fullington,Michael Dean; Goertemiller,Scott Allen, Method and system for exporting flight data for long term storage.
Bertin Olivier,FRX ; Levy-Abegnoli Eric,FRX, Method and system for selecting path according to reserved and not reserved connections in a high speed packet switchin.
Kettering, Christopher B.; Moore, Daniel B.; Hunter, Freelon F.; Toolson, Jeffery L.; Royalty, Charles D.; Jacobs, Michael N., Methods and apparatus providing an airborne e-enabled architecture as a system of systems.
Kawano,Satoshi; Nakajima,Hidekazu; Azuma,Yoichi; Kimura,Mitsumaro; Takahashi,Nobuo, Optimized path establishment method and network management system using the method.
McKenna, Daniel Bernard; Cruz, Joseph M.; Jochim, Kenneth Joseph; Varadachari, Anand K.; Saroka, Harold Grant; Liu, Dandan, System for integrating an airborne wireless cellular network with terrestrial wireless cellular networks and the public switched telephone network.
Malreddy, Muralidhar; Talley, Ryan; Narendran, Rajveen, Use of pre-handoff macro-carrier data for prioritization of carriers in femtocell frequency-hopping pilot beacons.
Colella, Nicholas J.; Chadwick, George G., Wireless communication system, apparatus and method using an atmospheric platform having a wideband trunkline.
Wright Thomas H. ; Ziarno James J., Wireless frequency-agile spread spectrum ground link-based aircraft data communication system having adaptive power control.
Wright Thomas H. ; Salati Bruce D., Wireless spread spectrum ground link-based aircraft data communication system with airborne airline packet communications.
Wright Thomas H. ; Salati Bruce D., Wireless spread spectrum ground link-based aircraft data communication system with approach data messaging download.
Wright Thomas H. ; Ziarno James J., Wireless, frequency-agile spread spectrum ground like-based aircraft data communication system with remote flight operations control center.
Wright, Thomas H.; Ziarno, James J., Wireless, frequency-agile spread spectrum ground link-based aircraft data communication system with wireless unit in communication therewith.
Wright, Thomas H.; Ziarno, James J., Wireless, frequency-agile spread spectrum ground link-based aircraft data communication system with wireless unit in communication therewith.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.