Abstract: Integrated communications apparatus and methods are used to receive, transmit, and operate on communications signals. A composite semiconductor structure may be formed for providing an integrated communications device that may include transceiver circuitry, data converter circuitry, and processor circuitry. The data converter circuitry may include an analog-to-digital and/or digital-to-analog data converter that is implemented at least partly using compound semiconductors (e.g., using compound semiconductor transistors for implementing comparators and/or switches in the data converter). The processor circuitry may include some circuitry that is formed from non-compound semiconductors, which is better suited than compound semiconductors to perform digital signal processing operations. The transceiver circuitry may include compound and/or non-compound semiconductor circuitry depending on the signal frequency and whether the signal is optical or electrical.

Abstract: A monolithic, software-definable, power amplifier is provided. According to one embodiment of the invention, power amplifier circuits can be tuned to the most efficient power amplification characteristics as determined by a digital microprocessor based on varying data. The data may relate to user density, carrier frequency and spectral band. The power amplifier circuits may also be formed on semiconductor structures that include monocrystalline silicon substrates and layers of monocrystalline compound semiconductors. In these structures, the power amplifier may be integrated in a single integrated circuit wherein portions of the power amplifier circuits may be formed on the silicon substrate and portions may be formed on the compound semiconductor. This configuration may substantially increase efficiency of the integrated power amplifier according to the invention.

Abstract: A zero-drift constellation (200 FIG. 2) is used to simplify the tracking and hand-off requirements of terrestrial-based user terminals (110 FIG. 1). Each satellite (120 FIG. 1) traces out a common ground track which has a number of southbound segments and an equal number of adjacent northbound segments. This allows user terminals (110) to employ antennas with only one degree of freedom to track satellites (120) in zero-drift constellation (200). User terminals (110) perform hand-offs with satellites (120) that are within a limited field of view with respect to user terminal (110). User terminal (110) tracks a first satellite until a crossover point is reached and then performs a hand-off to a second satellite traveling in the opposite direction along an adjacent segment. User terminal (110) tracks the second satellite until another crossover point is reached and then performs a hand-off to a third satellite traveling in the same direction as the first satellite along an adjacent segment.

Abstract: A mechanical scanning and digital beamforming antenna (20, FIG. 2) uses a receive and transmit digital beamforming network (FIG. 3, 410, 320) to provide communications beam scanning in a first plane. In a second plane, a reflective surface (FIG. 2, 240) is used to focus and scan the communications beam. Through proper orientation of the reflective surface (240), a communications satellite (FIG. 1, 10) can be tracked by way of electronic scanning by way of the transmit or receive digital beamforming network (FIG. 3, 320, 410). Thus, the complexity of the digital beamforming network is reduced as is the wear on the mechanical components of the antenna. The mechanical scanning and digital beamforming antenna (20, FIG. 20) makes use of a second digital beamforming network (FIG. 3, 415, 325) and reflective surface (FIG. 3, 250) to ensure that two communications satellites can be simultaneously tracked.