A multi-mode communication adapter system comprising: a mobile Earth station including: a flat panel antenna configured to receive a down-link satellite packet, wherein the flat panel antenna includes a waveguide interposer, a satellite Rx/Tx, coupled to the flat panel antenna, configured to decode the down-link satellite packet, a storage device, coupled to the satellite Rx/Tx, configured to store satellite data from the down-link satellite packet, a first interface module, coupled to the storage device, configured to encode and transfer the satellite data as a cellular communication packet, a second interface module, coupled to the storage device, configured to encode and transfer the satellite data as a WiFi packet, and a multi-band transceiver, coupled to the first interface module and the second interface module, configured to concurrently transfer the cellular communication packet and the WiFi packet without accessing a local infrastructure; and a protective cover encloses the mobile Earth station.

Systems, apparatuses, methods, and software are described herein that provide enhanced satellite communication nodes. In one example, a parent communication node is configured to establish a satellite edge network over at least a satellite communication pathway with a child communication node remotely located from a geographic location of the parent node. The child communication node is configured to communicate over at least the satellite communication pathway to establish a connection to the satellite edge network and route communications of a local communication interface to the satellite edge network.

The disclosed technology relates to systems and methods for tasking satellite constellations. A method is disclosed herein for receiving, from a resource database of a satellite control system, knowledge data corresponding to a plurality of components associated with a satellite constellation communications system. The plurality of components can include one or more satellites associated with a constellation. The method includes processing the knowledge data according at least one received mission objective. Processing the knowledge data can include determining a status of at least one satellite in the constellation. The method includes scheduling the satellite control system based at least in part on the received mission objective and the processed knowledge data; initiating communication with the at least one satellite in the constellation according to the scheduling; receiving updated status information for at least one component of the plurality of components; and storing, in the resource database, the updated status information.

A constellation configuration optimization method of a low earth orbit (LEO) satellite augmentation system for an ARAIM application includes: 1, traversing vertical protection levels after all subset solutions and fault modes under the condition that integrity risk and continuity risk are equally distributed, and determining the constraint conditions of LEO satellite constellation configuration parameters; 2, determining objective functions of LEO satellite constellation configuration parameters x.sub.1, x.sub.2, x.sub.3, x.sub.4, eliminating calculated values of abnormal vertical protection levels, and screening initial populations of the parameters x.sub.1, x.sub.2, x.sub.3, x.sub.4; 3, calculating fitness of the objective functions; 4, starting from a second generation population, merging a parent population with an offspring population to form a new offspring population; 5, performing local optimal selection on the new offspring population, screening out a maximum value of the objective functions as an optimal offspring, and repeating step 4 until a genetic algebra is less than a maximum genetic algebra.

A method and apparatus for non-terrestrial network beam switching is provided. A non-terrestrial network base station includes a transmitter configured to transmit downlink data to user equipment and a receiver configured to receive uplink data from the user equipment. A channel bandwidth of the non-terrestrial network base station is divided into a plurality of bandwidth parts respectively corresponding to a plurality of geographic areas, and each bandwidth part is respectively associated with a satellite beam. When the user equipment is located in a first geographic area, the transmitter transmits the downlink data to the user equipment over a corresponding first bandwidth part. After the user equipment transitions from the first geographic area to a second geographic area, the transmitter transmits the downlink data to the user equipment over a corresponding second bandwidth part of the plurality of bandwidth parts.

In a method and apparatus for inter-satellite communications, transmissions between a satellite and neighboring satellites that share an orbital plane occur via an aft antenna or a forward antenna and transmissions between the satellite and neighboring satellites that do not share an orbital plane occur via the aft antenna or the forward antenna timed during orbital plane crossings. This occurs even if the total path length and number of links is higher than inter-satellite communications that use side-to-side transfers.

A satellite communication method includes communicating with a user equipment UE via an inter-satellite link or an intra-satellite link by a core network using a first communication satellite; and communicating with a service server via the inter-satellite link or the intra-satellite link by the core network. The service server and the core network may be on the same or different satellites. A satellite apparatus, core network element and storage medium are also discussed.

In one implementation, a system for space-based aircraft monitoring includes a ground segment, multiple aircraft monitoring payloads on board corresponding satellites, and a resource scheduling system. Individual payloads include antenna systems configured to provide multiple beams for receiving ADS-B messages and two or more receivers configured to process received ADS-B messages that are implemented, at least in part, by reconfigurable FPGAs. In addition, individual payloads are configured to initiate transmission of ADS-B messages processed by one or more of their receivers to the ground segment. Meanwhile, the ground segment is configured to receive such messages and to route them to one or more destinations for aircraft monitoring. The resource scheduling system is configured to control the antenna systems of individual payloads to dynamically adjust the beams for receiving ADS-B messages of the individual antenna systems.

Satellites provide communication between devices such as user terminals and gateways to other networks, such as the Internet. Non-geosynchronous orbit satellites move relative to terrestrial user terminals, passing in and out of communication over time. To maintain ongoing communication, a handover takes place in which the responsibility to maintain communication with a particular user terminal passes from one satellite to another. To minimize disruption due to the handover, satellite motion and availability of communication resources are allocated in advance. Participating devices such as the user terminal, current satellite, and next satellite, are provided with details of the handover in advance. As a result, interruption in communication due to a handover from one satellite to another is substantially reduced.

A method comprising determining, by a function, that a first satellite lacks processing or communication capabilities; and routing data traffic, by the function, from the first satellite to a second satellite, the second satellite having higher processing or communication capabilities than the first satellite. The processing and communication capabilities of the first and second satellite are directly related to their power availability, which is derived from solar energy means. Another method comprising determining, by a function, that a first satellite cannot provide computing or communication resources; migrating data, by the function, from the first satellite to a second satellite that can provide the computing or communication resources; computing the data, by the computing resources of the second satellite; and transmitting computed data, by the function, from the second satellite to the first satellite.