Abstract: Systems and methods for verifying the identities of RFID tags are provided. An RFID reader is configured to transmit an interrogation sequence to an RFID tag and recover digital information stored on the tag from an RFID response signal. A verification module is configured to extract a plurality of characteristics of the RFID response signal associated with Technically Uncontrollable RFID Features (TURF) of the RFID tag, and verify the identity of the RFID tag according to these characteristics.

Abstract: A machine for cleaning a window is provided which may comprise a chassis, window cleaning apparatus or mechanism, and a makeweight wherein the makeweight counterbalances the weight of the window cleaning apparatus by traversing the chassis in the first and second directions as the cleaning apparatus traverses the chassis in the second and first directions, respectively.

Abstract: A pod propulsion system comprises a housing defining a fluid duct and an annular drum rotatably mounted to the housing within the fluid duct. The annular drum has a drum interior and a cylindrical outer surface. The system further comprises a rotor mounted to the drum for rotation therewith, the rotor and the drum having a common axis of rotation. A bearing assembly mounted to the housing comprises a first bearing comprising a first plurality of bearing pads disposed circumferentially around the drum. Each pad has a pad bearing surface adapted to contact a first drum portion in a predetermined manner and is pivotably mounted to the housing so as to maintain contact of the pad bearing surface with the first drum portion in the predetermined manner when an orientation of the drum portion relative to the housing changes.

Abstract: The invention is sensor pod assembly for mounting sensor systems for an aircraft, the aircraft having a fuselage with a longitudinal axis. In detail the sensor pod includes an elongated pod having front and rear ends, the pod removable mountable to the underside of the fuselage of the aircraft aligned with the longitudinal axis. A mounting system is includes to mount at least one container capable of being pressurized in a plurality of locations within the pod along the longitudinal axis, the at least one container including means to mount the sensor systems there within.

Abstract: An aircraft motion control mechanism for regulating aircraft motion from a location remote from an aircraft body portion. The aircraft auxiliary control mechanism has at least one control surface support arm connected to and extending from the aircraft body portion, and an auxiliary flow control surface connected to the support arm. By pivotally controlling the movement of the support arm, the auxiliary flow control surface is operative to deflect airflow to regulate orientation of the aircraft. In addition, the auxiliary flow control surface may further deflect the airflow by deflecting about the support arm.

Abstract: A method for fabricating nanocoils and improved nanocoils fabricated therefrom. Embodiments of the method utilizing deep reactive ion etching (DRIE). A method for fabricating nanocoils includes providing a silicon-on-insulator (SOI) wafer, in which SOI wafer includes buried oxide layer, patterning one or more devices into a layer of silicon on top of the buried oxide layer, depositing tensile stressed nitride layer on the top silicon layer, patterning coiling arm structure on top silicon layer, patterning an overlapping etch window mask on bottom side of SOI wafer using, in which patterning overlapping etch window mask removes SOI wafer and exposes buried oxide layer in width greater than coiling arm structure, and releasing coiling arm structure so that coiling arm coils to form nanocoil. In embodiments, DRIE is utilized to pattern the overlapping etch window mask.

Abstract: A method of assembling a first part and a second part. The method includes the step of integrally forming an attachment device and a first part. For example, the attachment device may be a nut plate operative to retain a nut therein, and the first part may be an air duct. The nut plate and the air duct may be integrally formed via selective laser sintering or stereo lithography such that the nut plate is an integral feature of the air duct. A nut may be retained in the nut plate, and a mating bolt may engage the nut to attach the air duct (i.e., the first part) to the second part.

Abstract: An electrical power feed thru for thin-walled vessels such as aircraft fuselages is disclosed which allows high electrical current power lines, and their associated high operating temperatures, to transition from the inside to the outside of the aircraft. The feed thru includes sealing surfaces, anti-rotation features and safety covers. This low-profile configuration permits the attached cables to run close to the fuselage walls, permitting easier routing and clamping. The feed thru has a variable geometry which permits alternate spacing of the end terminations in reference to the fuselage while maintaining the same parts. Installation is simplified through a single fuselage wall mounting hole design that can be done with a standard punch. The feed thru exceeds the shock and vibration environments of various aircraft such as a military aircraft.

Abstract: A light-powered data acquisition and control system immune to electromagnetic interference employs smart sensors in a network configuration capable of decentralized communication. A smart sensor with integral transducer encloses a microprocessor, fiber optic transceiver, and photovoltaic converter within a Faraday cage. Optical fibers link plural sensors for duplex communication with a fiber optic splitter, which transmits high intensity light to the converter for powering the sensors. The sensor converts analog input from the transducer into bit packets for fiber optic transmission to the network via the splitter. Firmware in the splitter converts the bit packets to network protocol and vice versa enabling data communication among sensors, splitters, and control receivers. Verification algorithms for testing sensors are run automatically by the microprocessor or through commands issued via the network. Mnemonics stored in the sensors provide automatic updating of system configuration.

Abstract: Systems are disclosed for providing substantially equal E-plane and H-plane radiation patterns in a high power and dual band coaxial feedhorn antenna for a satellite communication system. One embodiment may include a coaxial feedhorn antenna comprising an outer coaxial horn portion for propagation of first signals and an inner horn portion for propagation of second signals. The coaxial feedhorn antenna may also comprise a conductive choke-ring coupled to the outer conductive wall, the conductive choke-ring being coaxial with the outer coaxial horn portion and the inner horn portion. The conductive choke-ring provides substantially equal E-plane and H-plane radiation patterns of the first signals and substantially reduced back-lobes.

Abstract: An autonomous air vehicle comprises a flight control system and an automatic contingency generator for automatically determining a contingent air vehicle route for use by the flight control system in response to contingencies experienced by the air vehicle. A method of automatically determining the contingent air vehicle route is also provided.

Abstract: Methods and apparatus for: (a) the correction of one or more elements determined from a first set of continuous gyro and accelerometer measurements comprising using a second set of discontinuously measured higher accuracy accelerometer measurements doubly integrated in an inertial coordinate system, (b) determining relative movement of a vehicle using a first set of acceleration measurements that do not include components of acceleration caused by the Earth's gravitational field, and a second set of acceleration measurements that do include components of acceleration caused by the Earth's gravitational field; and (c) correcting errors in an inertial navigation system positioned in a vehicle comprising using independently measured changes in position of the vehicle relative to an inertial coordinate frame.

Abstract: The present invention provides a navigation system for an unmanned underwater vehicle that includes at least two navigation sensors that provide latitude and longitude measurements of unequal accuracy, a processor and a memory. The memory stores a machine-readable set of instructions executable by the processor to process the latitude and longitude measurements received from the navigation sensors, and to estimate vehicle latitude and longitude with approximately equal accuracy.

Abstract: A technique and tool are provided for repairing damaged areas of honeycomb structures. The tool includes a plurality of rods axially translatable into the damaged area. Foam material is inserted about the rods and allowed to cure. The rods are later withdrawn leaving a porous core of material. Sleeves may be provided to receive and support the rods as they translate into the damaged area. The sleeves may remain in the damaged area after the rods are withdrawn into the sleeves.

Abstract: Distributed Aperture Systems use multiple staring sensors distributed around a vehicle to provide automatic detection of targets, and to provide an imaging capability at all aspects. The sensor image data is “stitched” to make the camera joints transparent to the operator. For example, images from three different cameras may be combined into a single seamless mosaic. The output mosaic is suitable for rendering on a head-steered helmet mounted display or a multifunction console display.

Abstract: An apparatus in one example has: a first component coupled to a second component by a suspension component; and the suspension component structured to maintain predetermined angular spring rates and to maintain high linear spring rates, that are higher than the angular spring rates, along linear axes of the suspension component that flex under predetermined increased dynamic loading of the suspension component.

Abstract: A software integration architecture is disclosed. The architecture includes software modules operative to spontaneously integrate distributed components/systems into new integrated systems via dynamic integration connectors, with minimal or no changes to the existing software components/systems/databases. The architecture employs integration rule sets that define access and communication rules associated with a respective software component, and a negotiation engine that negotiates with the integration connectors to define data and/or control connectivity based on the integration rule sets.

Abstract: In accordance with the present invention, there is provided a technique which may be used in conjunction with an automated Z-pin insertion process to automatically monitor the insertion energy applied to the Z-pins during the initial insertion phase of the automated insertion process, and compare it to an empirically derived value for good insertions, thereafter allowing the insertion process to continue to a predetermined additional insertion depth before terminating the process. The insertion energy is calculated by cumulatively summing the insertion force and multiplying it by the insertion time, thus yielding the cumulative energy. At a specified, predetermined insertion depth, the energy accumulation is stopped and the value at the initial insertion depth is stored and compared to an empirically derived value. If the value is less than the empirical value, the insertion energy is too low, thus indicating that either a partial grid insertion is being encountered or defective Z-pins are being inserted.

Abstract: Transistor devices are provided configured to operate at frequencies above a typical first cutoff frequency. In one aspect, a method is provided for configuring a transistor device to operate above a first cutoff frequency. The method comprises selecting a desired operating frequency range and a desired output power for a transistor associated with the transistor device, analyzing the effects of phase velocity mismatch on the overall gain of a plurality of different sized transistors, and evaluating the primary and secondary gain regions of the plurality of different sized transistors. The method further comprises selecting a transistor sized to provide the desired output power at or close to the desired operating frequency range based on the analysis of the phase velocity mismatch and the evaluation of the primary and secondary gain regions.

Abstract: A system is disclosed in which a geographic area of interest can be selected, and photographic images of the selected area can be downloaded and displayed by a user in an efficient and timely manner. The geographic area of interest may initially be selected by various input means such as a map, longitude/latitude coordinates, a global positioning system (GPS), and the like. Once the particular geographic area has been selected, photographic images corresponding to the selected area are downloaded to the user. The photographic images may be stored in a suitable data storage system such as a server. Alternatively, the photographic image data may be generated real time and downloaded to the user. In one embodiment, a relatively low resolution image of a large geographic area is initially displayed to the user, and the user can then select a limited region of the image for closer viewing.