In an exemplary embodiment, a phased array antenna comprises multiple subcircuits in communication with multiple radiating elements. The radio frequency signals are independently adjusted for both polarization control and beam steering. In a receive embodiment, multiple RF signals of various polarizations are received and combined into at least one receive beam output. In a transmit embodiment, at least one transmit beam input is divided and transmitted through multiple radiating elements, with the transmitted beams having various polarizations. In an exemplary embodiment, the phased array antenna provides multi-beam formation over multiple operating frequency bands. The wideband nature of the active components allows for operation over multiple frequency bands simultaneously.

Satellites in the direct-to-user Earth observation (EO) satellite system support inter-satellite communication and form a multihop communication network. Each satellite has a radio transceiver with a phased array antenna for directly communicating with a user radio station that issues an EO request of a user. Physical servers are distributed over the satellites and networked to form an in-space computer network that is Internet-enabled. The multihop communication network enables the servers to be mutually communicable. Raw data generated from the EO sensors are processed by the servers to yield desired EO data that meets the user's requirement. Advantageously, the servers set up a user authentication server configured to verify the user identity for determining acceptance or denial of the EO request, and an application server for interacting with the user. Hence, the EO request is entirely handled in Space without involving a terrestrial non-user facility for user authentication and raw-data processing.

Systems, methods, and apparatus for commercial satellite operations with secure enclave for payload operations are disclosed. In one or more embodiments, the disclosed method comprises generating, by a secure enclave of a host satellite operation center (SOC), hosted commands according to service specifications for at least one hosted user. The method further comprises generating, by a SOC operation portion of the host SOC, host commands according to service specifications for a host user. Also, the method comprises transmitting, by the host SOC, the host commands and the hosted commands to a vehicle. In addition, the method comprises reconfiguring a host/hosted payload on the vehicle according to the host commands and the hosted commands. Additionally, the method comprises generating, by the host/hosted payload, host telemetry and hosted telemetry. Also, the method comprises transmitting, by the vehicle, the host telemetry and the hosted telemetry to the host SOC.

A system includes a terminal and a gateway. The terminal is programmed to identify, in received data, a signature of rogue data that includes at least a device identifier and an application identifier, and to transmit, via uplink to a satellite, the identified signature to a gateway. The gateway is programmed to block downlink data, upon determining that downlink data includes the received signature, and to broadcast the received signature to a second gateway.

A radio communication route enables communication from an originating ground station to a destination ground station via one of multiple randomly orbiting, rotating satellites with no active attitude control. The ground stations and satellites include directional antennas for receiving radio signals from and transmitting radio signals in multiple directions. The satellites store an address of a destination ground station from which an initial information signal is transmitted and antenna information identifying the satellite antenna on which the initial information signal was received. Plural satellite antennas transmit linking information identifying the satellite to the originating ground station. Data transmissions received at the originating ground station that designate a particular destination are transmitted by the originating ground station using the antenna on which the linking information was received and the satellite retransmits the data transmission using the satellite antenna identified by the stored antenna information.

Systems, methods, and apparatus for commercial satellite operations with secure enclave for payload operations are disclosed. In one or more embodiments, the disclosed method comprises generating, by a secure enclave of a host satellite operation center (SOC), hosted commands according to service specifications for at least one hosted user. The method further comprises generating, by a SOC operation portion of the host SOC, host commands according to service specifications for a host user. Also, the method comprises transmitting, by the host SOC, the host commands and the hosted commands to a vehicle. In addition, the method comprises reconfiguring a host/hosted payload on the vehicle according to the host commands and the hosted commands. Additionally, the method comprises generating, by the host/hosted payload, host telemetry and hosted telemetry. Also, the method comprises transmitting, by the vehicle, the host telemetry and the hosted telemetry to the host SOC.

In an exemplary embodiment, a phased array antenna comprises multiple subcircuits in communication with multiple radiating elements. The radio frequency signals are independently adjusted for both polarization control and beam steering. In a receive embodiment, multiple RF signals of various polarizations are received and combined into at least one receive beam output. In a transmit embodiment, at least one transmit beam input is divided and transmitted through multiple radiating elements, with the transmitted beams having various polarizations. In an exemplary embodiment, the phased array antenna provides multi-beam formation over multiple operating frequency bands. The wideband nature of the active components allows for operation over multiple frequency bands simultaneously.

A radio communication route enables communication from an originating ground station to a destination ground station via one of multiple randomly orbiting satellites with no attitude control. The ground stations and satellites include directional antennas for receiving radio signals from and transmitting radio signals in multiple directions. The satellites store an address of a destination ground station from which an initial information signal is transmitted and antenna information identifying the satellite antenna on which the initial information signal was received. Plural satellite antennas transmit linking information identifying the satellite to the originating ground station. Data transmissions received at the originating ground station that designate a particular destination are transmitted by the originating ground station using the antenna on which the linking information was received and the satellite retransmits the data transmission using the satellite antenna identified by the stored antenna information.

In an exemplary embodiment, a phased array antenna comprises multiple subcircuits in communication with multiple radiating elements. The radio frequency signals are independently adjusted for both polarization control and beam steering. In a receive embodiment, multiple RF signals of various polarizations are received and combined into at least one receive beam output. In a transmit embodiment, at least one transmit beam input is divided and transmitted through multiple radiating elements, with the transmitted beams having various polarizations. In an exemplary embodiment, the phased array antenna provides multi-beam formation over multiple operating frequency bands. The wideband nature of the active components allows for operation over multiple frequency bands simultaneously.

Disclosed herein is a method for managing aeronautical safety-critical services or data links, comprising: receiving quality measurement data indicative of a quality parameter measured for an aeronautical safety-critical service or data link used by an aircraft; receiving a four-dimensional position associated with the quality measurement data, wherein said four-dimensional position includes a three-dimensional space position and a corresponding time that are computed based on a Global Navigation Satellite System and related to the measured quality parameter; tagging the quality measurement data with the associated four-dimensional position; determining, on the basis of the tagged quality measurement data and of a predefined task policy, a task to be performed, which task includes an adaptation of the aeronautical safety-critical service used by the aircraft or of resources allocated to the aeronautical safety-critical data link used by the aircraft, wherein said adaptation is based on said tagged quality measurement data; and performing the determined task.