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公开(公告)号：US20190280764A1
公开(公告)日：2019-09-12
申请号：US16422516
申请日：2019-05-24
Applicant: Vector Launch Inc.
Inventor： Shaun Coleman , Darren D. Garber
Abstract: Systems, methods, and software described herein provide enhancements for deploying software payloads in satellite systems. In one example, a satellite device comprises a communication interface configured to receive software payloads for execution, and an execution system configured to execute ones of the software payloads as associated virtual nodes that share resources of the satellite device to at least perform activities using one or more on-board systems of the satellite device. The execution system is configured to transfer state information related to execution of ones of the virtual nodes to at least another device over the communication interface, wherein the state information comprises data related to the activities.
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公开(公告)号：US20190253134A1
公开(公告)日：2019-08-15
申请号：US15892854
申请日：2018-02-09
Applicant: Vector Launch Inc.
Inventor： Shaun Coleman , John Metzger , Darren D. Garber
CPC classification number: H04B7/18519 , H04B7/18513 , H04B7/18521 , H04B7/18597 , H04W72/085
Abstract: Various enhanced operations and orbital techniques for satellite devices are discussed herein. In one example, a method of operating an orbital satellite platform is provided. The method includes establishing relative distances between a plurality of satellite devices, and performing temporary adjustments to the relative distances between the satellite devices. The method also includes directing at least communication processes among the satellite devices based at least in part on the temporary adjustments to the relative distances.
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公开(公告)号：US20190165852A1
公开(公告)日：2019-05-30
申请号：US16245420
申请日：2019-01-11
Applicant: Vector Launch Inc.
Inventor： Shaun B. Coleman , Darren D. Garber
Abstract: Systems, methods, and software described herein provide enhancements for deploying applications in spaceborne and airborne systems, among others. In one example, an airborne or spaceborne physical node comprises a communication interface configured to receive software payloads, and logistical control elements of the physical node. The physical node further comprises a virtualized execution system configured to execute ones of the software payloads deployed on the physical node as associated virtual nodes that share resources of the physical node.
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公开(公告)号：US10305582B2
公开(公告)日：2019-05-28
申请号：US16137862
申请日：2018-09-21
Applicant: Vector Launch Inc.
Inventor： Shaun Coleman , Darren D. Garber
Abstract: Systems, methods, and software described herein provide enhancements for deploying applications in satellite systems. In one example, a satellite system comprises a communication interface configured to receive software payloads, and logistical control elements of the satellite system. The satellite system further comprises a virtualized execution system configured to execute ones of the software payloads deployed on the satellite system as associated virtual nodes that share resources of the satellite system.
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公开(公告)号：US09991951B2
公开(公告)日：2018-06-05
申请号：US15626929
申请日：2017-06-19
Applicant: Vector Launch Inc.
Inventor： Shaun Coleman , Darren D. Garber
CPC classification number: H04B7/18519 , G06F9/45533 , G06F2009/4557 , G06K9/0063 , G06K9/00677 , G06K9/00979 , H04B7/18521 , H04L67/1068 , H04L67/125 , H04L67/34
Abstract: Systems, methods, and software described herein provide enhancements for deploying applications in satellites. In one example, a satellite device includes a communication interface and a virtualized execution system. The virtualized execution system is configured to receive state information via the communication interface from at least a peer satellite device related to execution of one or more software payloads by the peer satellite device, and execute one or more virtual nodes based at least on the state information.
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Patent Agency Ranking
公开(公告)号：US20180123681A1
公开(公告)日：2018-05-03
申请号：US15859978
申请日：2018-01-02
Applicant: Vector Launch Inc.
Inventor： Shaun Coleman , Darren D. Garber
CPC classification number: H04B7/18519 , G06F9/45558 , G06F2009/45579 , G06F2009/45583 , H04B7/18521 , H04L41/0668 , H04L67/10 , H04L67/1078 , H04L67/125 , H04L67/34
Abstract: Systems, methods, and software described herein provide enhancements for deploying applications in satellite systems. In one example, a satellite system comprises a communication interface configured to receive software payloads, and a satellite control system configured to operate logistical control elements of the satellite system. The satellite system further comprises a virtualized execution system configured to execute ones of the software payloads deployed on the satellite system as associated virtual nodes that share resources of the satellite system.
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公开(公告)号：US09722692B1
公开(公告)日：2017-08-01
申请号：US15297461
申请日：2016-10-19
Applicant: Vector Launch Inc.
Inventor： Shaun Coleman , Darren D. Garber
CPC classification number: H04B7/18519 , G06F9/45533 , G06F2009/4557 , G06K9/0063 , G06K9/00677 , G06K9/00979 , H04B7/18521 , H04L67/1068 , H04L67/125 , H04L67/34
Abstract: Systems, methods, and software described herein provide enhancements for deploying applications in satellites. In one example, a satellite may receive software applications capable of execution as virtual nodes on the satellite, and receive a resource schedule associated with the software applications. The satellite may further execute the software applications on the satellite based on the resource schedule, wherein the resource schedule allocates processing resources and user sensor resources to the software applications.
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公开(公告)号：US09641238B1
公开(公告)日：2017-05-02
申请号：US15297436
申请日：2016-10-19
Applicant: Vector Launch Inc.
Inventor： Shaun Coleman , Darren D. Garber
CPC classification number: H04B7/18519 , G06F9/45558 , G06F2009/45579 , G06F2009/45583 , H04B7/18521 , H04L41/0668 , H04L67/10 , H04L67/1078 , H04L67/125 , H04L67/34
Abstract: Systems, methods, and software described herein provide enhancements for deploying applications in satellites. In one example, a satellite may receive software applications capable of execution as virtual nodes on the satellite, and receive a resource schedule associated with the software applications. The satellite may further execute the software applications on the satellite based on the resource schedule, wherein the resource schedule allocates processing resources and user sensor resources to the software applications.
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公开(公告)号：US10659564B2
公开(公告)日：2020-05-19
申请号：US16422584
申请日：2019-05-24
Applicant: Vector Launch Inc.
Inventor： Shaun Coleman , Darren D. Garber
Abstract: Systems, methods, and software described herein provide enhancements for computing platforms. In one example, a computing device is configured to maintain attribute scoring metrics that rate target computing devices in competency among at least a portion of roles defined at least by presently provisioned software elements and hardware elements. The computing device is configured to identify tasks to be serviced using one or more of the roles, and based at least in part on the attribute scoring metrics, determine one or more target computing devices that satisfy the one or more of the roles to handle the tasks. The computing device is configured to transfer at least task instructions for delivery to the one or more target computing devices for performing the tasks using at least one among the presently provisioned software elements and hardware elements associated with the one or more of the roles.
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公开(公告)号：US10536107B1
公开(公告)日：2020-01-14
申请号：US16156170
申请日：2018-10-10
Applicant: Vector Launch Inc.
Inventor： Andrew Daichi Ning , George Lewis Teel , Brian James Riskas , Darren D. Garber
IPC: H02S10/40 , H01M10/46 , H02S40/38 , H02J7/35 , H01M10/0525 , H01M10/625 , B64G1/42 , B64G1/10 , B64G1/44 , H01M10/615
Abstract: Various enhanced power supply configurations for satellite devices are discussed herein. In one example, satellite device includes a chassis and a power control module. The satellite device also includes an array of polygonal-shaped power units combined into a geometric arrangement by disposing the polygonal-shaped power units around the power control module within the chassis. In some examples, the polygonal-shaped power units comprise a rhomboid chassis or enclosure that provides arrangement into a hexagonal array when coupled to eight further rhomboid power units. Other polygonal arrays can be formed using arrangements of the repeating polygonal-shaped power units.
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