公开(公告)号：US20240253826A1

公开(公告)日：2024-08-01

申请号：US18152273

申请日：2023-01-10

申请人： Network Access Associates Limited (a private company incorporated in England and Wales, with company

发明人： John GUINEY ,  Daniel John KROBOTH ,  Hank TSEU

IPC分类号： B64G3/00 ,  B64G1/24 ,  G06F3/0484 ,  G06Q10/0631

CPC分类号： B64G3/00 ,  B64G1/24 ,  G06F3/0484 ,  G06Q10/06316

摘要： Systems and methods of the present disclosure may use a satellite operations center (SOC) to determine a satellite anomaly indicative of a problem with a health or status of satellite. The SOC may generate a satellite anomaly ticket recording the satellite anomaly, space environment context data and satellite telemetry data and append the satellite anomaly ticket to a ticket queue in a ticket buffer. The SOC may instruct, upon the satellite anomaly ticket being in a first position in the ticket queue, an interface management service to render, on a display of a terminal, a user interface to enable the operator to address the satellite anomaly ticket via user interactions. The SOC may generate a workflow of tasks to address the satellite anomaly ticket based on the user interactions, and instruct the fleet operations ground segment element to perform the tasks and generate a satellite command to the satellite.

公开(公告)号：US20240199241A1

公开(公告)日：2024-06-20

申请号：US18426390

申请日：2024-01-30

申请人： Purple Mountain Observatory, Chinese Academy of Sciences

发明人： Jin XU ,  Zhibin CAO ,  Kejun LIU ,  Jianli DU ,  Jianbo MA ,  Dong YANG

IPC分类号： G01S17/66 ,  B64G3/00 ,  G01S13/86 ,  G01S13/933 ,  G01S17/87 ,  G01S17/933

CPC分类号： G01S17/66 ,  B64G3/00 ,  G01S13/865 ,  G01S13/933 ,  G01S17/87 ,  G01S17/933

摘要： In a search and tracking method for full time-domain laser detection of space debris, a set of latest precision orbital parameters of a debris object and start and end moments of a current transit of the object are first obtained. Search-specific guidance data is generated based on the above information and in combination with estimation of a maximum along-track error of the orbital parameters of the object during the current transit. A DLR system performs multi-elevation search on the object based on the search-specific guidance data, obtains a plurality of pieces of detection data of the object after detecting the object during the search, determines an along-track error of the orbital parameters of the object based on the detection data, and corrects the orbital parameters of the object in real time based on the along-track error, so as to guide the DLR system to subsequently track and detect the object.

公开(公告)号：US20240174384A1

公开(公告)日：2024-05-30

申请号：US18523749

申请日：2023-11-29

申请人： Korea Aerospace Research Institute

发明人： Youeyun Jung ,  Okchul Jung ,  Jaedong Seong ,  Saehan Song ,  Myeongshin Lee ,  Daewon Chung

IPC分类号： B64G1/24 ,  B64G3/00 ,  G06T7/70 ,  G06T17/00 ,  H04L9/40

CPC分类号： B64G1/244 ,  B64G3/00 ,  G06T7/70 ,  G06T17/00 ,  H04L63/105 ,  G06T2207/10032

摘要： Disclosed is a metaverse platform operating method and system for implementing a virtual universe space. The metaverse platform operating method includes: obtaining a plurality of satellite data from a satellite vehicle on a predetermined period for a predetermined time; constructing space situational awareness (SSA) information associated with the satellite vehicle by processing the plurality of satellite data; generating a metaverse-based virtual universe space in which the satellite vehicle is positioned for the predetermined time, through three-dimensional (3D) modeling of the SSA information; at an access request from a device, identifying a satellite-related organization to which the device belongs, using a login account included in the access request; and visualizing the metaverse-based virtual universe space on the device according to an information access right of the satellite-related organization.

公开(公告)号：US20240168193A1

公开(公告)日：2024-05-23

申请号：US18551047

申请日：2022-03-17

申请人： Share My Space

发明人： Damien Giolito ,  Romain Lucken

IPC分类号： G01V8/00 ,  B64G3/00 ,  G06T7/20

CPC分类号： G01V8/00 ,  B64G3/00 ,  G06T7/20 ,  G06T2207/30241

摘要： A system for detecting the path of moving objects, comprises telescopes rotating in an azimuthal plane and each oriented with an elevation angle between 30° and 85°, each of the telescopes having a field of view between 2 and 6 degrees square and comprising a sensor of N×M pixels each of a width L. The system comprises a computer for storing time-stamped images delivered by the sensor of each of the telescopes and for computing the path of a celestial object depending on luminous traces of the celestial object in a first image and in a second image.

公开(公告)号：US20240158104A1

公开(公告)日：2024-05-16

申请号：US18499567

申请日：2023-11-01

申请人： Georgia Tech Research Corporation

发明人： Mehregan Dor ,  Travis Driver ,  Panagiotis Tsiotras

IPC分类号： B64G1/24 ,  B64G3/00 ,  G01C21/24 ,  G06T7/73 ,  G06V20/56 ,  G06V20/64

CPC分类号： B64G1/247 ,  B64G3/00 ,  G01C21/24 ,  G06T7/73 ,  G06V20/56 ,  G06V20/64 ,  G06T2200/04 ,  G06T2207/10032 ,  G06T2207/30252

摘要： An exemplary system and method are disclosed for a standalone vision-based system for autonomous online navigation, e.g., around an unknown target small body. The exemplary system (also referred to as AstroSLAM) is predicated on the formulation of the SLAM problem as an incrementally growing factor graph. Using the GTSAM library and the iSAM2 engine, the exemplary system and method combine sensor fusion with the prior orbital motion to provide navigation and parameter estimation that improves the performance over a baseline SLAM implementation. The exemplary system and method can incorporate orbital motion constraints into the factor graph by devising a relative dynamics factor that can link the relative pose of the spacecraft to the problem of predicting trajectories stemming from the motion of the spacecraft in the vicinity of the small body.

公开(公告)号：US20240140618A1

公开(公告)日：2024-05-02

申请号：US18280476

申请日：2022-03-29

申请人： Mitsubishi Electric Corporation

发明人： Hisayuki MUKAE

IPC分类号： B64G1/10 ,  B64G3/00

CPC分类号： B64G1/1028 ,  B64G1/1085 ,  B64G3/00

摘要： A surveillance satellite that has detected a significant high luminance generates launch sensing data indicating a launch time point corresponding to a detection time point, a launch coordinate value expressing a position at which the significant high luminance was detected, and a line-of-sight vector at the detection time point and containing surveillance data at the detection time point and transmits the launch sensing data. A communication satellite that passes through a point in a communication range with respect to the surveillance satellite to transmit the launch sensing data receives the launch sensing data and transmits the launch sensing data to remaining communication satellites via a satellite communication network.

公开(公告)号：US20230382567A1

公开(公告)日：2023-11-30

申请号：US17828819

申请日：2022-05-31

申请人： The Aerospace Corporation

发明人： Mohammad MOZUMDAR ,  Phanitta CHOMSINSAP ,  Sadiq SARWAR

IPC分类号： B64G3/00 ,  B64G1/10 ,  H04L9/00

CPC分类号： B64G3/00 ,  B64G1/1085 ,  H04L9/50

摘要： A framework for interfacing a blockchain-based ground system with flight software and satellite orbit analysis applications is disclosed. A blockchain application (e.g., a web application) for secure management of satellites has three components—a client, a server, and a private and permissioned-based blockchain network (e.g., a Hyperledger Fabric™ network). The client allows users to configure satellite parameters. The server facilitates the communication between the client and the blockchain. The blockchain allows the secure management and storage of satellite configuration data on blockchain ledgers. For instance, SECCON provides a blockchain-based framework that can be a potential candidate for next generation ground system applications. SECCON allows secure configuration management of satellites, and has been interfaced with OpenSatKit, a software tool kit that can interact with the cFS. SECCON also provides secure communication of orbital data between trusted organizations and allows the satellite configuration parameters to be exported and viewed in SOAP.

公开(公告)号：US20230166873A1

公开(公告)日：2023-06-01

申请号：US17933602

申请日：2022-09-20

申请人： Utah State University Space Dynamics Laboratory

发明人： Skylar Cox ,  Justin Whitaker ,  John Humble ,  Greg Droge

IPC分类号： B64G3/00 ,  G06F9/48

CPC分类号： B64G3/00 ,  G06F9/4881 ,  B64G1/1007

摘要： For generating a points-of-interest plan, a method generates communication graph nodes for at least one satellite. The method calculates communication graph edges from the communication graph nodes, wherein the communication graph nodes and the communication graph edges comprise a communication graph. The method solves the communication graph to yield a communication plan. The method generates a points-of-interest plan from the communication plan.

公开(公告)号：US11661218B2

公开(公告)日：2023-05-30

申请号：US16324537

申请日：2017-08-08

申请人： ispace, inc.

发明人： Takeshi Hakamada ,  Takahiro Nakamura ,  John Walker ,  Toshiro Shimizu ,  Toshiki Tanaka ,  Daisuke Furutomo ,  Yu Kudo ,  Kiyona Miyamoto ,  Daishi Matsukura ,  Mohamed Ragab ,  Abdelkader Haouchine ,  Damien Haikal ,  Chit Hong Yam ,  Julian Jakub Gramatyka

IPC分类号： B64G5/00 ,  E21C51/00 ,  B64G1/10 ,  B64G1/16 ,  B64G1/42 ,  B64G1/44 ,  B64G1/66 ,  B64G3/00 ,  C25B1/04 ,  H04N5/265 ,  H04N5/225

CPC分类号： B64G5/00 ,  B64G1/105 ,  B64G1/1085 ,  B64G1/16 ,  B64G1/421 ,  B64G1/443 ,  B64G1/66 ,  B64G3/00 ,  C25B1/04 ,  E21C51/00 ,  H04N5/265 ,  B64G2001/1071 ,  H04N5/2253

摘要： An exploration method includes: a step of exploring a natural resource on a satellite, a minor planet, or a planet; a step of acquiring the natural resource detected by the exploration; and a step of storing the acquired natural resource.

公开(公告)号：US11574223B2

公开(公告)日：2023-02-07

申请号：US16595107

申请日：2019-10-07

申请人： INTELLIGENT FUSION TECHNOLOGY, INC.

发明人： Dan Shen ,  Carolyn Sheaff ,  Jingyang Lu ,  Genshe Chen ,  Erik Blasch ,  Khanh Pham

IPC分类号： G06N7/00 ,  B64G3/00 ,  G06N20/00

摘要： A method for rapid discovery of satellite behavior, applied to a pursuit-evasion system including at least one satellite and a plurality of space sensing assets. The method includes performing transfer learning and zero-shot learning to obtain a semantic layer using space data information. The space data information includes simulated space data based on a physical model. The method further includes obtaining measured space-activity data of the satellite from the space sensing assets; performing manifold learning on the measured space-activity data to obtain measured state-related parameters of the satellite; modeling the state uncertainty and the uncertainty propagation of the satellite based on the measured state-related parameters; and performing game reasoning based on a Markov game model to predict satellite behavior and management of the plurality of space sensing assets according to the semantic layer and the modeled state uncertainty and uncertainty propagation.