Abstract: Systems and methods for determining absolute position. A system includes a first bull gear and a second bull gear rigidly connected to the first bull gear. The system includes a first pinion gear rotationally engaged with the first bull gear. The system includes a second pinion gear rotationally engaged with the second bull gear. The system includes a first sensor that senses a first angular position of the first pinion gear. The system includes a second sensor that senses a second angular position of the second pinion gear.

Abstract: Embodiments of the invention include an integrated monopulse comparator assembly for use in tracking antenna applications such as an antenna feed or an antenna array. Embodiments of the monopulse comparator assembly may include four rectangular waveguide antenna inputs, four magic tees, rectangular waveguide connections, and four rectangular waveguide monopulse outputs. An embodiment of a 4×4 antenna array including an embodiment of an integrated monopulse comparator assembly is also disclosed.

Abstract: Embodiments of the invention include an integrated single-piece antenna feed and a turnstile circular polarizer suitable for use in a satellite communications system. One embodiment of the integrated single-piece antenna includes a circular waveguide input, a turnstile, a coaxial feed horn, subreflector and subreflector support. Alternative embodiments utilize symmetrically oriented struts with or without a coaxial subreflector support to physically support a subreflector.

Abstract: Embodiments of the invention include an integrated monopulse comparator assembly for use in tracking antenna applications such as an antenna feed or an antenna array. Embodiments of the monopulse comparator assembly may include four rectangular waveguide antenna inputs, four magic tees, rectangular waveguide connections, and four rectangular waveguide monopulse outputs. An embodiment of a 4×4 antenna array including an embodiment of an integrated monopulse comparator assembly is also disclosed.

Abstract: Embodiments of the invention include an integrated single-piece antenna feed and a turnstile circular polarizer suitable for use in a satellite communications system. One embodiment of the integrated single-piece antenna includes a circular waveguide input, a turnstile, a coaxial feed horn, subreflector and subreflector support. Alternative embodiments utilize symmetrically oriented struts with or without a coaxial subreflector support to physically support a subreflector.

Abstract: Embodiments of the invention include an integrated single-piece antenna feed and a turnstile circular polarizer suitable for use in a satellite communications system. One embodiment of the integrated single-piece antenna includes a circular waveguide input, a turnstile, a coaxial feed horn, subreflector and subreflector support. One embodiment of the turnstile features four branches of wrapped-single-ridged waveguide. Another embodiment is a turnstile circular polarizer.

Abstract: Embodiments of the invention include an integrated single-piece antenna feed and a turnstile circular polarizer suitable for use in a satellite communications system. One embodiment of the integrated single-piece antenna includes a circular waveguide input, a turnstile, a coaxial feed horn, subreflector and subreflector support. One embodiment of the turnstile features four branches of wrapped-single-ridged waveguide. Another embodiment is a turnstile circular polarizer.

Abstract: The invention is an integrated single-piece antenna feed, turnstile polarizer and antenna system suitable for satellite communications. One embodiment of the integrated single-piece antenna includes a circular waveguide input, a circular polarizer, a coaxial feed horn, subreflector and subreflector support. One embodiment of the circular polarizer features four branches of wrapped-single-ridged waveguide.

Abstract: According to the invention, a method for determining the radial position of a rotatable object is disclosed. The method may include providing targets at known relative radial positions coupled with the object, where a radial distance between any two adjacent targets is substantially not equal to the radial distance between any other two adjacent targets. The method may also include rotating the object about an axis, where the distance of the rotation is believed to be known. The method may further include determining, during rotation, that a first target is in proximity to a point fixed relative to the axis. The method may additionally include determining, during rotation of the object, that a second target is at least in proximity the point fixed relative to the axis. The method may moreover include comparing of the believed known rotation with the known relative radial positions of the plurality of targets.