Abstract: An apparatus for use in inspecting a wire segment is provided. The apparatus includes a guide tube sized to receive the wire segment, and an array of mirrors positioned about the guide tube. Each mirror in the array is oriented such that a reflection of the wire segment in the array of mirrors forms a circumferential view of at least a portion of the wire segment, and such that the reflection from each mirror is within a field of view from a single vantage point.

Abstract: Systems capable of acquiring polarimetry data using a single camera with or without a polarizing filter. When a polarizing filter is used, the data acquisition method comprises: (1) maneuvering the aircraft (or other vehicle) to orient the polarizing filter (and camera) in various directions when images are captured, (2) registering the various images to each other, and (3) computing polarimetry values (such as the Stokes parameters) for points of interest in the images. When a polarizing filter is not used, the data acquisition method comprises maneuvering the aircraft (or other vehicle) to orient the camera in various directions when images are captured and then performing the same operations (2) and (3). These methods measure the amount of polarization in a given scene by taking multiple camera images at different angles.

Abstract: An apparatus for directing thermal infrared energy toward or away from a target is disclosed. The apparatus comprises a covering having a plurality of retroreflective elements. The plurality of retroreflective elements are configured to retroreflect electromagnetic beams primarily at thermal infrared wavelengths, receive the electromagnetic beams from the target along beam reception paths, and reflect the electromagnetic beams back toward the target along beam reflection paths. The beam reflection paths have substantially the same elevation angle and/or azimuth angle as their respective beam reception paths.

Abstract: Systems and methods for mitigating constraints associated with wireless power transmission in applications where the position and orientation of the desired magnetic field changes over time, for example, because the position and orientation of the receiver being powered changes over time or because different receivers having different positions and orientations are being powered at different times. In accordance with some embodiments, the system employs a plurality of wireless power transmitters in a defined space, each transmitter consisting of individual coils oriented orthogonally relative to each other. Using field interference amongst these individual coils as well as amongst the transmitters they form, one can actively control the wireless power field intensity and orientation at any given point in the defined space. This allows for methods to steer the power transmission towards a specific target at a specific angle.

Abstract: A method for capturing hyperspectral images using a regular color camera. In the method, the camera takes multiple images of a scene, with the camera oriented differently for each image. For a camera carried by an aircraft or spacecraft, this allows hyperspectral imaging without the cost or weight of a hyperspectral camera.

Abstract: A method and apparatus for operating an electric motor is presented. A transmit magnetic field is received at a group of receive coils having a group of axes oriented substantially parallel to magnetic field lines from a transmit coil and having a group of resonant frequencies. A resonant frequency in the group of resonant frequencies is different from other receive coils in the group of receive coils. A receive magnetic field is generated at a receive coil in the group of receive coils having the resonant frequency when the transmit magnetic field has a selected frequency matching the resonant frequency. The receive magnetic field attracts a rotor in the electric motor.

Abstract: A deployable vortex generator attached to a lifting surface includes a vane moveable relative to the lifting surface. The vane moves from a deployed position to a retracted position in response to a change in ambient conditions. In the deployed position, the vane acts on the air flow to create vortices. In the retracted position, the vane is closely aligned with the free stream velocity.

Abstract: A method of controlling the shape and direction of an explosion may include embedding a plurality of detonators in an explosive, and arranging the detonators in the explosive to produce a shaped explosion of the explosive in a pre-set direction and having a pre-set intensity when triggered in a selected sequence; sensing a direction of an incoming threat relative to a protected region, calculating an intercept vector for the incoming threat, and sending a signal in response thereto by a sensor; receiving information from the sensor pertaining to the intercept vector and determining a sequential firing pattern for the detonators in response to the information from the sensor by a firing sequence calculator connected to trigger the detonators; and activating the firing sequence calculator to trigger the detonators in the sequential firing pattern to generate a counteracting force substantially along the intercept vector.

Abstract: A method and apparatus for managing a location. Soil sensor units are deployed in the location in a forest from a group of aerial vehicles. Information is generated about a number of soil conditions in the location in the forest using the soil sensor units in the location. The information is transmitted from the soil sensor units to a remote location for analysis.

Abstract: A method of controlling the shape and direction of an explosion may include embedding a plurality of detonators in an explosive, and arranging the detonators in the explosive to produce a shaped explosion of the explosive in a pre-set direction and having a pre-set intensity when triggered in a selected sequence; sensing a direction of an incoming threat relative to a protected region, calculating an intercept vector for the incoming threat, and sending a signal in response thereto by a sensor; receiving information from the sensor pertaining to the intercept vector and determining a sequential firing pattern for the detonators in response to the information from the sensor by a firing sequence calculator connected to trigger the detonators; and activating the firing sequence calculator to trigger the detonators in the sequential firing pattern to generate a counteracting force substantially along the intercept vector.

Abstract: Ground support equipment that makes it easier to monitor the electrochemical health of a battery. This ground support equipment is configured to implement methods for estimating the total volume and the free volume of liquid electrolyte in an electrochemical cell or in a battery containing several electrochemical cells. The methods involve measuring a center of gravity and/or a moment of inertia. The systems include ground-support equipment suitable for use in aircraft maintenance.

Abstract: An air vehicle may include a body having forwardly-swept fixed wings or unswept fixed wings. The body may have a longitudinal axis continuously oriented parallel to a forward flight direction when the air vehicle is in flight. The air vehicle may include at least one of the following components being mounted on opposite sides of the body: longitudinally offset engine nacelles, asymmetrically lengthened engine nacelles, and longitudinally offset protruding aerodynamic surfaces comprising at least one of stabilizers, canards, empennage control surfaces, external stores, and high aspect ratio wings.

Abstract: A method and apparatus for controlling an electric motor. Power is transmitted to windings of the electric motor by wireless magnetic coupling between transmission coils and the windings.

Abstract: Systems capable of acquiring polarimetry data using a single camera with or without a polarizing filter. When a polarizing filter is used, the data acquisition method comprises: (1) maneuvering the aircraft (or other vehicle) to orient the polarizing filter (and camera) in various directions when images are captured, (2) registering the various images to each other, and (3) computing polarimetry values (such as the Stokes parameters) for points of interest in the images. When a polarizing filter is not used, the data acquisition method comprises maneuvering the aircraft (or other vehicle) to orient the camera in various directions when images are captured and then performing the same operations (2) and (3). These methods measure the amount of polarization in a given scene by taking multiple camera images at different angles.

Abstract: A turbulence and winds aloft detection system may include an image capturing device for capturing a plurality of images of a visual feature of a selected celestial object; and an image processor configured to compare the plurality of images of the visual feature to detect a transit of a turbule of turbulent air between the image capturing device and the selected celestial object; compensate for one or more of apparent visual motion of celestial objects due to a planet's translation and rotation, the moon's revolution about the planet, and the atmosphere's refractive displacement of celestial objects; and compute a measurement of at least one of a velocity of the turbule and a height of the turbule relative to the planet.

Abstract: A method and apparatus for strike detection. Images of an object are identified in video images from a video camera on a vehicle. A movement of the object with respect to the vehicle is identified from the images of the object in the video images. It is determine whether the movement of the object with respect to the vehicle indicates that the object will strike the vehicle. A strike report comprising information indicating that the object will strike the vehicle is generated in response to a determination that the object will strike the vehicle.

Abstract: An unmanned aerial vehicle (UAV) includes at least one passive reflective device having an elongated configuration defining a long axis and comprising a material configured to reflect radio signals. The UAV also includes a control system configured to control the UAV along a flight path that orients the at least one passive reflective device such that the long axis remains substantially tangential to an ellipsoid whose foci are at two points between which radio communication is desired.

Abstract: A system for detecting volcanic plumes using a camera on an aircraft, a distant point-like source of light, and a computerized method of processing images acquired by the camera to detect phenomena indicative of the presence of volcanic plumes in a volume of space intersected by light from the light source. A computer system is programmed to determine whether the image data from the camera has characteristics indicating that the imaged light had passed through a volcanic plume or not. In response to detection of a volcanic plume in the flight path of an aircraft, the computer system outputs an alert activation signal to an alert device that produces a visible or audible alert.

Abstract: A method and apparatus for identifying a position of a surface on an aircraft. Image data for an image of the surface on the aircraft is received. The image data is processed to determine whether the position of the surface on the aircraft is a desired position. A surface position identification report comprising information identifying whether the position of the surface on the aircraft is the desired position is generated.

Abstract: A method and system for attenuating a shockwave propagating through a first medium by heating a selected region of the first fluid medium rapidly to create a second, transient medium that intercepts the shockwave and attenuates its energy density before it reaches a protected asset. The second medium may attenuate the shockwave by one or more of reflection, refraction, dispersion, absorption and momentum transfer. The method and system may include a sensor for detecting a shockwave-producing event, determining a direction and distance of the shockwave relative to a defended target and calculating a firing plan, and an arc generator for creating the second medium. The arc generator may create the second medium by creating an electric arc that travels along an electrically conductive path utilizing at least one of high intensity laser pulses, pellets forming a conductive ion trail, sacrificial conductors, projectiles trailing electrical wires, and magnetic induction.