Abstract: A multifunction peripheral (MFP) includes user selectable functions that call home applications on the device that direct it to work cooperatively with cloud service providers. To avoid requiring users to login to each cloud service each time they use it, they are registered with an authorization server to establish and grant identity and authorization tokens. When a user logs in to an MFP, they are redirected to login to the authorization server which then sends tokens to the MFP identifying the user and their permissions and licenses. Home applications associated by the tokens are displayed for selection. Each time a home application using a cloud service is selected, a background application sends the user's session tokens with a service request to an associated cloud service resource server. The resource servers processes authenticated requests and return the result to the MFP which completes the selected home application function.

Abstract: Methods and systems for satellite payloads are provided. A first system is based on using a focal plane array tiles with a reflector. A second system uses active lens tiles, focal plane array tiles and the reflector. A third system includes active reflector tiles, focal plane array tiles and the reflector. Yet another system enables beam power sharing by selectively providing power to solid state power amplifiers used in satellite payloads. Another system uses multiple micro-satellites for providing satellite coverage for an area.

Abstract: Methods and systems for satellite payloads are provided. A first system is based on using a focal plane array tiles with a reflector. A second system uses active lens tiles, focal plane array tiles and the reflector. A third system includes active reflector tiles, focal plane array tiles and the reflector. Yet another system enables beam power sharing by selectively providing power to solid state power amplifiers used in satellite payloads. Another system uses multiple micro-satellites for providing satellite coverage for an area.

Abstract: An aeronautical satellite broadband communications system has an antenna defined by a transmit gain pattern varying according to an orientation relative to a geostationary orbit satellite. An antenna controller unit is connected to an aircraft inertial navigation system and receptive to navigation data therefrom, and a set of antenna orientation data is derived from the navigation data on a real-time basis. A broadband controller connected to the antenna controller unit generates a set of output variables as a function of normalized equivalent isotropic radiated power spectral density values of the antenna and the set of antenna orientation data. The set of output variables controls the output power and carrier bandwidth of transmissions from the antenna within predefined limits of equivalent isotropic radiated power spectral density that vary with values of the set of antenna orientation data.

Abstract: A system and method for communicating information from a base station to one or more user terminals via a forward link to a relay and distribution device is provided. The method includes determining a separate information rate for information to be transmitted from the base station to each of the user terminals. Each information rate is determined to allow successful communication with the respective user terminal and to provide a predetermined amount of link margin above a threshold energy-to-noise ratio (Eb/No) in the forward link. The method additionally includes formatting data received at the base station into a continuous time division multiplexed (TDM) data stream that includes a plurality of data frames to be transmitted to the user terminals. Each data frame is formatted to have the determined information rate of the respective user terminal destine to receive the data frame. The TDM data stream is transmitted using a single carrier of the forward link.

Abstract: An apparatus and method for correcting antenna beam misalignment between a transmit antenna and a receive antenna on a mobile platform such as an aircraft. The beam alignment method makes use of sequential lobing to determine the pointing angles in azimuth and elevation of a receive beam received by the receive antenna. For the transmit antenna, sequential lobing is used for the transmit antenna beam transmitted to a transponded satellite and then to a ground station. The ground station performs received signal strength indicator (RSSI) measurements and transmits these measurements back to the aircraft 16 via the target satellite. From these measurements, the beam misalignment between the receive and transmit antenna beams, both in azimuth and elevation, can be determined and a correction applied to the transmit antenna.