Abstract: A passive sensing system for determining a physical position of a mechanical device includes an encoding system configured to convert a position signal representative of the physical position of the mechanical device into an encoded signal in a binary format. The sensing system also comprises a plurality of secondary optical paths coupled to a primary optical path positioned between a light source and the encoding system. The encoded signal comprises a plurality of pulses of light each sequentially delayed by the secondary optical paths. A system for determining a physical position of a flight control surface of an aircraft is also disclosed. A method for determining a physical position of a flight control surface of an aircraft is also disclosed. A passive sensing system for determining a physical position of a flight control surface of an aircraft is also disclosed.

Abstract: A method and apparatus for capturing and processing images from a portion of a system in order to detect a warning condition for providing warnings to users or operators of the system. One or more image capture devices capable of capturing an image, for example, a continuous video, monitor at least a portion of the system. An image processing assembly processes the image captured by the image capture devices in real time for determining if the warning condition exists. Upon determining that the warning condition exists the image processing assembly causes a warning device to provide a warning to the user. The captured image may then be displayed to the user or operator if desired.

Abstract: A system and method for enhancing the integrity of a system which uses a high performance, low assurance, general purpose microprocessor to execute an avionics software application and uses a high assurance, low performance microprocessor to monitor the output of the general purpose microprocessor, without the need for comparison of outputs from parallel processors executing functionally equivalent versions of the avionics software application. The monitoring microprocessor is used to analyze state transitions of the first microprocessor and to analyze the computed values output by said general purpose microprocessor, against predetermined limitations based upon aircraft limitations.

Abstract: A method and apparatus for fabricating a complex, three-dimensional structure (12), such as a truss, from composite fiber/resin includes pulling a plurality of continuous fibers (50) from a feed source (62) along a processing path (58) about a longitudinal axis (14). At least some of the fibers are wound around the longitudinal axis in opposite directions (70,72) by rotational elements to form helical and reverse helical components (30, 34) that intersect at nodes (26,28). Select nodes are engaged by engagement members (84) and are maintained radially outwardly from the longitudinal axis by a support frame (80) to create sequential discrete segments (22) in the helical and reverse helical components. The select nodes can be engaged and maintained from outside the helical and reverse helical components. Resin can be applied to the fibers by resin applicator (90) and cured.

Abstract: A block code for correcting adjacent errors and almost-adjacent errors that occur in semiconductor memory data, with such errors possibly being caused by a neutron single event upset (NSEU). A block code includes a generator matrix that has columns in which an exclusive-or of adjacent or almost-adjacent columns provides a unique value for each of the possible combination of columns of the generator matrix. As such, a computed syndrome can be used to effectively correct for any adjacent errors and almost-adjacent errors, as well as double-adjacent errors, double-adjacent errors, and triple-almost-adjacent errors.

Abstract: A multiple virtual machine system with a microprocessor for executing instructions and issuing memory reads and writes to a current partition of a plurality of partitions. The multiple virtual machine may contain a partition management unit for receiving the memory reads and writes from the microprocessor for the current partition. A current partition cache is selected by the partition management unit for the current partition to receive the current partition memory reads and writes from the partition management unit. The current partition cache resolves memory read hits and misses. A next partition cache is selected by the partition management unit when the next partition becomes active on the microprocessor to receive next partition memory reads and writes from the microprocessor.

Abstract: A single event upset (SEU) resistant semiconductor circuit element and a method of making are provided by the invention. The single event upset resistant semiconductor circuit element includes a plurality of parallel-connected semiconductor cell elements. Each semiconductor cell element of the plurality of parallel-connected semiconductor cell elements is physically separated from the other cell elements. Moreover, the semiconductor cell elements may be physically separated by at least one intervening semiconductor cell element of another circuit element.

Abstract: A structural member having greatly enhanced load bearing capacity per unit weight has a plurality of helical components wrapped around a longitudinal axis. The helical components have straight segments rigidly connected end to end in a helical configuration. In a basic repeating unit, three helical components have a common angular orientation, a common longitudinal axis, and are spaced apart from each other at equal distances. Another three reverse helical components also have a common angular orientation, a common longitudinal axis, and are spaced apart from each other at equal distances, but have an opposing angular orientation. These six helical components appear as a triangle when viewed along the axis due to the straight segments. An additional six helical are configured as above but rotated with respect to the first six components such that the member appears as a six-pointed star when viewed from the axis.

Abstract: In an internal combustion engine having two or more coplanar cylinders radially disposed about a crankshaft, a crankshaft journal bearing arrangement in which the big ends of the connecting rods are each formed as segments of a continuous circular bearing for assembly about a single crankshaft journal. The big end of each connecting rod comprises an internal arcuate bearing segment and concentric external bearing segments. When assembled about the crankshaft journal, the external bearing segments are encircled by two containment rings whereby the internal arcuate bearing segments are maintained in operational engagement with the crankshaft journal. The containment rings are fixed for rotation with the crankshaft and relative sliding movement between the containment rings and the assembled connecting rod big ends occurs at the external bearing segments.