An antenna orientation deciding method in a wireless communication system that has a communication device provided with an antenna having directionality and a relay device that travels, includes a deciding step of deciding an orientation at which the directionality of the antenna as to the relay device is optimal, on the basis of position information of the communication device, orbit information of the relay device, and information relating to orientation of directionality of the antenna.

An antenna orientation deciding method in a wireless communication system that has a communication device provided with an antenna having directionality and a relay device that travels, includes a deciding step of deciding an orientation at which the directionality of the antenna as to the relay device is optimal, on the basis of position information of the communication device, orbit information of the relay device, and information relating to orientation of directionality of the antenna.

A method for satellite communication over non-geosynchronous orbit (NGSO) satellites, using a terminal having a non-tracking antenna, is presented. The terminal may communicate with an NGSO satellite each time the NGSO satellite passes through the terminal's antenna beam (communication opportunity). Though the communication opportunities are short and may reoccur at relatively long intervals (e.g., minutes to tens of minutes), these communication opportunities may be sufficient for transmitting the volumes of information generated by Internet of Things (IoT) applications during the intervals between communication opportunities.

A method for satellite communication over non-geosynchronous orbit (NGSO) satellites, using a terminal having a non-tracking antenna, is presented. The terminal may communicate with an NGSO satellite each time the NGSO satellite passes through the terminal's antenna beam (communication opportunity). Though the communication opportunities are short and may reoccur at relatively long intervals (e.g., minutes to tens of minutes), these communication opportunities may be sufficient for transmitting the volumes of information generated by Internet of Things (IoT) applications during the intervals between communication opportunities.

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.

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.

A method and system for finding the true geolocation coordinates of User Equipment (UE) using a communication network and system based on Non-Terrestrial Network (NTN). The system uses precision clock signals of a UE and satellites in an NTN. Using the time of arrival method disclosed in the invention, a trusted satellite can compute the location of a UE by processing positioning signals. Consequently, satellites accurately compute the true location of UE and store it on satellites in the space and/or database server connected with the ground station. The invention enables accurate delivery of shipments in a logistic network.

A method and system for finding the true geolocation coordinates of User Equipment (UE) using a communication network and system based on Non-Terrestrial Network (NTN). The system uses precision clock signals of a UE and satellites in an NTN. Using the time of arrival method disclosed in the invention, a trusted satellite can compute the location of a UE by processing positioning signals. Consequently, satellites accurately compute the true location of UE and store it on satellites in the space and/or database server connected with the ground station. The invention enables accurate delivery of shipments in a logistic network.

A device for the reception of ADS-B messages for a satellite is disclosed including an array of sources and a beamforming module, a ground footprint of a field of view defining a service area, different service areas being associated with different positions of the satellite, a ground footprint of a beam defining a spot in the service area, the beamforming module being configured to form each beam by applying combination coefficients, the reception device having a processing circuit configured to obtain information representative of a position of the satellite and to modify a set of combination coefficients so as to adapt the surface area and/or or the shape of the formed spots to a geographical distribution of the aircrafts within the service area associated with the position of the satellite.

A device for the reception of ADS-B messages for a satellite is disclosed including an array of sources and a beamforming module, a ground footprint of a field of view defining a service area, different service areas being associated with different positions of the satellite, a ground footprint of a beam defining a spot in the service area, the beamforming module being configured to form each beam by applying combination coefficients, the reception device having a processing circuit configured to obtain information representative of a position of the satellite and to modify a set of combination coefficients so as to adapt the surface area and/or or the shape of the formed spots to a geographical distribution of the aircrafts within the service area associated with the position of the satellite.