Abstract: An apparatus for providing automatic gain control for use in a satellite terminal of a satellite communication system capable of transmitting a plurality of different modes of data. The apparatus includes a demodulator circuit having an analog to digital converter; a first variable attenuator having an attenuation value set on the basis of a measured power level of a predetermined data signal; and a second variable attenuator having an attenuation value set on the basis of the mode of data being received by the satellite terminal, where each of the data modes have a corresponding predetermined attenuation value associated therewith which is utilized as the attenuation value of the second variable attenuator when the satellite terminal receives the data mode.

Abstract: An apparatus for transmitting and receiving signals over a two-way satellite communication system is disclosed. A receiving unit receives data from a user terminal. A transmitting unit is coupled to the receiving unit and transmits the data to an antenna. The data is transmitted over a return channel that is established over the satellite to a hub; the hub has connectivity to a packet switched network.

Abstract: A method of terminating two or more constituent encoders of a turbo encoder employing a turbo code, comprising the step of: generating tail input bits at each of two or more constituent encoders, including deriving the tail input bits from each of the two or more constituent encoders separately from a contents of shift registers within each of the two or more constituent encoders, after an encoding of information bits by the two or more constituent encoders; puncturing one or more tail output bits such that 1/R output tail bits are transmitted for each of a plurality of trellis branches, wherein R is a turbo code rate employed by the turbo encoder during an information bit transmission. In yet another variation, the step of puncturing the tail output bits further comprises the step of: transmitting, during trellis termination, the tail output bits, only if they are sent from an output branch of one of the two or more constituent encoders that are used during information bit transmission.

Abstract: A digital signal detection system, method and computer program product, including (a) partitioning a digital signal into a plurality of frames; (b) calculating a number of zero crossings of the digital signal within each frame; (c) determining whether or not an absolute value of a difference of the number of zero crossings in between frames is less than a first predetermined value; (d) determining whether or not a sum of the zero crossings of the frames is greater than or equal to a second predetermined value and less than or equal to a third predetermined value; (e) calculating a maximum amplitude of the digital signal for each of the frames; (f) calculating an average amplitude of the digital signal for all of the frames; (g) determining whether or not an absolute value of a difference between the maximum amplitude of a frame and the average amplitude is less than a fourth predetermined value times the average amplitude for each of the frames; and (h) determining that a frame contains a narrowband digital s

Abstract: A fault detection system for a satellite communication system includes a satellite positioned above earth. Satellite has a payload that communicates with a network control center on earth. System ground stations generate diagnostic messages and transmits the diagnostic messages to the payload. Each diagnostic message has a predetermined path characteristic so that the diagnostic message takes a predetermined path through the payload, or part of the payload, if the payload is operating properly. Parts of the payload, if any, which do not permit deterministic path tracing using externally applied diagnostic messages may be probed by using internal signal or data injection points. In response to the externally applied or internally injected diagnostic message, a response signal is generated at the payload. The response signal is transmitted to the network control center where it is compared with a predetermined response.

Abstract: The present invention is described by an electronic program guide with a calendar tool, and a method and apparatus for transmitting and receiving the electronic program guide. The apparatus includes a transmission station and a plurality of receiver stations. The transmission station creates program guide data that is in an “object” format. The transmission station combines the program guide objects with digital audio and video television signals, and transmits an output stream to the plurality of receiver stations. Each of the plurality of receiver stations stores electronic program guide objects. Using data from the electronic program guide objects, the plurality of receiver stations generate a listing of television program representations, and a calendar image separate from and adjacent to the plurality of television program representations.

Abstract: A spacecraft protected by a coating comprises a spacecraft having an external surface, and a coating on the external surface of the spacecraft. The coating includes a binder that is an organic material or an inorganic material, and a plurality of pyroelectric pigment particles bound together by the binder. The coating initially includes a coating vehicle which is subsequently evaporated so that the coating is a solid. The coating has a thickness of from about 0.001 inch to about 0.020 inch where the binder is an organic material, and has a thickness of from about 0.001 inch to about 0.010 inch where the binder is an inorganic material.

Abstract: A system in which a personal computer sends messages into a TCP/IP network using a conventional dial-up link and downloads data from the TCP/IP network using a high-speed one-way satellite link. A preferred embodiment uses a conventional SLIP provider to connect to the TCP/IP network and uses a commercial software TCP/IP package that has a standard driver interface. A spoofing protocol compensates for the long propagation delays inherent to satellite communication.

Abstract: A chip-on-board electronic device includes an electronic device die affixed to a printed circuit board, and electrically interconnected thereto by wirebonds. The electronic device is protected by coating it with a layer of silicon oxynitride and, optionally, an overlying thin layer of a conformal coating such as parylene. Under some circumstances, a protective layer of an organic material may be used instead of the layer of silicon oxynitride. The chip-on-board electronic device may be protected with an overlying layer of the conformal coating.

Abstract: A system for testing an embedded processor, such as an embedded processor for a spacecraft. The system comprises an Emulated Spacecraft Control Processor (ESCP) which contains the embedded processor, a simulation engine, and a host computer. The emulated spacecraft control processor includes a dual-port memory for emulating the memory for the embedded processor and data transfer logic which monitors cycles of the embedded processor to arbitrate access to the dual-port memory, the data transfer logic is operative to allow an access to the dual-port memory when the embedded processor performs an I/O cycle, wherein the access is performed before a subsequent machine cycle of the embedded processor.

Abstract: A compensation circuit and method for compensating for the threshold shift in an irradiated MOSFET. The method determines the gate threshold voltage to body voltage relationship to vary the body voltage with radiation. The compensation circuit has at least one MOSFET having the same channel type as the MOSFET being compensated. The at least one matching MOSFET is connected to the gate of the MOSFET being compensated. At least one MOSFET having a channel type that is different from the channel type of the MOSFET being compensated is connected to the gate of the matching MOSFET. The result is that the compensation circuit controls a negative shift in the body voltage of the MOSFET being compensated resulting in a higher threshold voltage.

Abstract: A conformally coated structure includes a component of an electronic assembly, such as a microelectronic device, a part of a package, or an electrically conductive trace, and a conformal coating applied to a surface of the structure. The conformal coating is a cured polymer blend of a base polymer and an electrically conductive polymer. The polymer blend has an electrical resistivity of from about 109 to about 1013 ohm-centimeter. The polymer blend contains from about 0.5 percent to about 4 percent by weight of the electrically conductive polymer, with the remainder the base polymer. The electrically conductive polymer may be a polyaniline, and the base polymer may be a urethane.

Abstract: A redundant microwave system operable to process a microwave signal propagating in a microwave cavity includes a microwave cavity and two microwave processing devices. Each microwave processing device has a transmissive impedance when it is on and a reflective impedance when it is off. There is a separate coupling probe extending from each of the microwave processing devices to locations within the microwave cavity. When a primary one of the microwave processing devices is switched on and the redundant microwave processing device is switched off, its coupling probe reflects energy so that almost all of the energy flows through the primary microwave processing device. If the primary microwave processing device fails and is switched off, its coupling probe reflects energy so that almost all energy flows through the redundant device. No separate active switching device or circuit is used.

Abstract: A traveling wave tube is coupled to an output waveguide by an output coupler. The output coupler includes a single integral hollow termination body having an inner surface and an outer surface. The slow-wave propagation structure of the traveling wave tube is joined to the inner surface of the hollow termination body such that the electron beam of the traveling wave tube passes through the interior of the single integral hollow termination body. The output waveguide contacts the outer surface of the opposite end of the single integral hollow termination body with an interference fit.

Abstract: A system and method for correcting pointing errors induced by an inclined orbit (14) for a satellite (20) that is adapted to be in an orbit having zero inclination (12). The present invention generates a yaw correcting cosine rate command (34) that is integrated (36) by a steering law having input parameters dependent upon the angle of inclination, &THgr;, to derive a sinusoidal yaw offset. The present invention also generates a roll correcting cosine rate command (54) that is integrated (56) according to a steering law having input parameters dependent upon the angle of inclination, &THgr;, to derive a sinusoidal roll offset.

Abstract: A microwave microstrip/waveguide transition structure includes a substrate, an elongated microstrip layer residing on a surface of the substrate, and an elongated integral hollow waveguide on the surface of the substrate. The microstrip layer and a side of the hollow waveguide constitute a single continuous piece of metal. The transition structure is fabricated by providing a substrate, depositing a metallic layer on the substrate, and depositing a metallic hollow housing continuous with a portion of a length of the metallic layer. The metallic hollow waveguide bounded by the metallic layer and the metallic hollow housing and having a contained volume therewithin is thereby defined.

Abstract: A packaged electronic structure includes an electronic device, and a package to which the electronic device is affixed. At least a portion of the package is made of a composite material of aluminum nitride dispersed in aluminum. The composite material is preferably prepared by mixing powders of the aluminum nitride and aluminum, and thereafter pressing and sintering the mixture.

Abstract: A satellite broadcast system and method, particularly useful for television signals, allows for local as well as nationwide broadcast service by allocating greater satellite resources to the more important local service areas. This is accomplished by broadcasting a non-uniform pattern of local service beams and designing the system to establish different service area priorities through factors such as the individual beam powers, sizes, roll-off characteristics and peak-to-edge power differentials. Frequency reuse is enhanced by permitting a certain degree of cross-beam interference, with lower levels of interference established for the more important service areas.

Abstract: A satellite broadcast system and method, particularly useful for television signals, allows for local as well as nationwide broadcast service by allocating greater satellite resources to the more important local service areas. This is accomplished by broadcasting a non-uniform pattern of local service beams and designing the system to establish different service area priorities through factors such as the individual beam powers, sizes, roll-off characteristics and peak-to-edge power differentials. Frequency reuse is enhanced by permitting a certain degree of cross-beam interference, with lower levels of interference established for the more important service areas.

Abstract: A satellite broadcast system and method, particularly useful for television signals, allows for local as well as nationwide broadcast service by allocating greater satellite resources to the more important local service areas. This is accomplished by broadcasting a, non-uniform pattern of local service beams and designing the system to establish different service area priorities through factors such as the individual beam powers, sizes, roll-off characteristics and peak-to-edge power differentials. Frequency reuse is enhanced by permitting a certain degree of cross-beam interference, with lower levels of interference established for the more important service areas.