Abstract: Systems and methods for aircraft refueling with sun glare prevention. One embodiment is a method that includes calculating a future time to position a receiver aircraft via an optical sensor with respect to a supply aircraft for an aerial fuel transfer, and calculating a sun position relative to the position of the receiver aircraft for the future time. The method also includes determining that the optical sensor of the receiver aircraft is susceptible to solar interference for the future time based on the sun position relative to the position of the receiver aircraft. The method further includes generating a request for the supply aircraft to move to an alternate position for the future time, and positioning the receiver aircraft via the optical sensor at the future time with respect to the alternate position of the supply aircraft for the aerial fuel transfer.

Abstract: A reconfigurable optical device includes a spatial light modulator and an optical signal generator. The spatial light modulator includes a layer of optically-sensitized carbon nanotubes, and each optically-sensitized carbon nanotube is configured to transition between a conductive state and a semiconductive state responsive to an optical signal. The optical signal generator is configured to provide the optical signal to the spatial light modulator to cause the layer of optically-sensitized carbon nanotubes to form a pattern of conductive nanotubes, the pattern of conductive nanotubes configured to modify interfering signal to form an optical vortex.

Abstract: A reconfigurable optical device includes a spatial light modulator and an optical signal generator. The spatial light modulator includes a layer of optically-sensitized carbon nanotubes, and each optically-sensitized carbon nanotube is configured to transition between a conductive state and a semiconductive state responsive to an optical signal. The optical signal generator is configured to provide the optical signal to the spatial light modulator to cause the layer of optically-sensitized carbon nanotubes to form a pattern of conductive nanotubes, the pattern of conductive nanotubes configured to modify interfering signal to form an optical vortex.

Abstract: Systems and methods for aircraft refueling with sun glare prevention. One embodiment is a method that includes calculating a future time to position a receiver aircraft via an optical sensor with respect to a supply aircraft for an aerial fuel transfer, and calculating a sun position relative to the position of the receiver aircraft for the future time. The method also includes determining that the optical sensor of the receiver aircraft is susceptible to solar interference for the future time based on the sun position relative to the position of the receiver aircraft. The method further includes generating a request for the supply aircraft to move to an alternate position for the future time, and positioning the receiver aircraft via the optical sensor at the future time with respect to the alternate position of the supply aircraft for the aerial fuel transfer.

Abstract: Configurable passive electromagnetic reflectors are disclosed, as are aircraft comprising configurable passive electromagnetic reflectors and methods to use configurable passive electromagnetic reflectors. In one embodiment a system comprises a reflector comprising a surface having a plurality of addressable patches switchable between a reflective state and a non-reflective state, and a controller coupled to the reflector to provide signals to switch the plurality of addressable patches between the non-reflective state and the reflective state to configure the reflector to selectively reflect incident electromagnetic radiation toward a remote target. Other embodiments may be described.

Abstract: A method for correcting for optical channel bandwidth misalignment between output passbands of a first optical device and input passbands of a second optical device. The method may involve transmitting a plurality of optical signals from the output passbands of the first optical device, with each of the optical signals being transmitted within an associated one of the passbands of the output. The first plurality of optical signals may be received within the input passbands of the second optical device. The optical signals may be analyzed to determine if the passbands of the first optical device or the second optical device has shifted. A characteristic of a filter through which the optical signals pass may be altered to cause a needed degree of shifting of wavelength bands of the optical signals to bring the optical signals into alignment within the passbands of the second optical device.

Abstract: An EMI-resistant control device for providing a control signal may include an optical glass fiber connector housing adapted to be connectable to an apparatus for providing the control signal to the apparatus for controlling operation thereof. The EMI-resistant control device may also include a carbon nanotube optical switch mounted in the optical glass fiber connector housing. The carbon nanotube optical switch may include a plurality of light sensitive carbon nanotubes adapted to connect a voltage source to an output of the EMI-resistant control device in response to an optical signal being received by the optical glass fiber connector housing. The optical glass fiber connector housing directs the optical signal onto the plurality of light sensitive carbon nanotubes. The voltage source provides the control signal to the apparatus.

Abstract: Apparatus and methods provide for the use of a lift-producing body with a landing gear assembly in order to provide a lifting force during landing gear operations that reduces the load on the landing gear actuator. According to embodiments, the lift-producing body may be configured for attachment to the landing gear assembly. The lift-producing body may be reconfigured while the landing gear assembly is being retracted or deployed in order to maximize the aerodynamic lift created by the lift-producing body or to minimize the drag induced by the lift-producing body.

Abstract: Optically reconfigurable radio frequency antennas for use in aircraft systems and methods of its use are disclosed. In one embodiment, the antenna includes a surface-conformal reflector that includes optically addressable carbon nanotubes. The nanotubes can be combined with light-sensitive materials so that exposure to light of the correct wavelength will switch the nanotubes back and forth between a metallic and non-metallic state. The antenna has a transmitter that radiates a radio frequency signal in the direction of the surface illuminator and an addressable optical conductor to illuminate the nanotubes with one or more optical signals. When the domains are illuminated they switch portions of the carbon nanotubes between its non-metallic states and metallic states to reflect the radiated radio frequency signal.

Abstract: An apparatus for establishing an optical circuit path spanning a discontinuity in an optical channel supported by a first cable oriented about a first axis on a first side of the discontinuity and supported by a second cable section oriented about a second axis on a second side of the discontinuity includes: (a) a first coupling member coupled with the optical channel on the first side; (b) a first supporting member fixed with the first coupling member in an installed orientation in a clamping relation with the first cable section; (c) a second coupling member coupled with the optical channel on the second side; (d) a second supporting member fixed with the second coupling member in an installed orientation clamped with the second cable section; and (e) a connecting member optically coupling the first coupling member with the second coupling member to establish the optical circuit path.

Abstract: Optically reconfigurable radio frequency antennas for use in aircraft systems and methods of its use are disclosed. In one embodiment, the antenna includes a surface-conformal reflector that includes optically addressable carbon nanotubes. The nanotubes can be combined with light-sensitive materials so that exposure to light of the correct wavelength will switch the nanotubes back and forth between a metallic and non-metallic state. The antenna has a transmitter that radiates a radio frequency signal in the direction of the surface illuminator and an addressable optical conductor to illuminate the nanotubes with one or more optical signals. When the domains are illuminated they switch portions of the carbon nanotubes between its non-metallic states and metallic states to reflect the radiated radio frequency signal.

Abstract: An EMI-resistant control device for providing a control signal may include an optical glass fiber connector housing adapted to be connectable to an apparatus for providing the control signal to the apparatus for controlling operation thereof. The EMI-resistant control device may also include a carbon nanotube optical switch mounted in the optical glass fiber connector housing. The carbon nanotube optical switch may include a plurality of light sensitive carbon nanotubes adapted to connect a voltage source to an output of the EMI-resistant control device in response to an optical signal being received by the optical glass fiber connector housing. The optical glass fiber connector housing directs the optical signal onto the plurality of light sensitive carbon nanotubes. The voltage source provides the control signal to the apparatus.

Abstract: An apparatus for establishing an optical circuit path spanning a discontinuity in an optical channel supported by a first cable oriented about a first axis on a first side of the discontinuity and supported by a second cable section oriented about a second axis on a second side of the discontinuity includes: (a) a first coupling member coupled with the optical channel on the first side; (b) a first supporting member fixed with the first coupling member in an installed orientation in a clamping relation with the first cable section; (c) a second coupling member coupled with the optical channel on the second side; (d) a second supporting member fixed with the second coupling member in an installed orientation clamped with the second cable section; and (e) a connecting member optically coupling the first coupling member with the second coupling member to establish the optical circuit path.

Abstract: A method for correcting for optical channel bandwidth misalignment between output passbands of a first optical device and input passbands of a second optical device. The method may involve transmitting a plurality of optical signals from the output passbands of the first optical device, with each of the optical signals being transmitted within an associated one of the passbands of the output. The first plurality of optical signals may be received within the input passbands of the second optical device. The optical signals may be analyzed to determine if the passbands of the first optical device or the second optical device has shifted. A characteristic of a filter through which the optical signals pass may be altered to cause a needed degree of shifting of wavelength bands of the optical signals to bring the optical signals into alignment within the passbands of the second optical device.

Abstract: A system and method for detecting and correcting for thermal shifting of the passbands of an input filter of an optical receiver relative to the passbands of an output of an optical device, such as an optical router, where the router and the receiver are operating at remote locations and at different operating temperatures that cause thermal drifting of the passbands. In one implementation RF signals are impressed on optical signals transmitted by a transmitter to the optical router. Different frequency RF signals are impressed on each of the optical signals and the receiver uses the detected RF frequencies to cancel portions of optical signals that have drifted into adjacent passbands at the optical receiver. In another implementation a mechanically adjustable filter is employed at the receiver which is used to achieve a needed degree of shifting of the receiver passbands to compensate for passband misalignment between the router and the receiver.

Abstract: Self-aligning optical connectors, systems, and methods for connecting optically-transmissive elements are described. In one embodiment, a connector includes a first component, a second component connected to the first component, and an optomechanical element. The optomechanical element is positioned adjacent and between said first and second components such that a portion of the optomechanical element is exposed to a leakage light when the first and second components are misaligned. The exposed portion includes a photosensitive material configured to at least attempt to change a dimension when exposed to the leakage light. In operation, the optomechanical element exerts an alignment force on at least one of the first and second components tending to align the first and second components when the exposed portion of the optomechanical element is exposed to the leakage light.

Abstract: Apparatus and systems described herein provide for a randomly-accessible electrical busbar with a protective cover and an associated mating connector. Both the busbar and the associated mating connector have multiple, electrically conductive bristles protruding from a surface. The busbar is protected by a nonconductive fabric cover to reduce the risk of a person from accidentally contacting the electrically conductive bristles. A connection is made between the mating connector and the busbar by the bristles of the mating connector penetrating the protective fabric cover and interdigitating with the bristles of the busbar.

Abstract: Apparatus and methods provide for the use of a lift-producing body with a landing gear assembly in order to provide a lifting force during landing gear operations that reduces the load on the landing gear actuator. According to embodiments, the lift-producing body may be configured for attachment to the landing gear assembly. The lift-producing body may be reconfigured while the landing gear assembly is being retracted or deployed in order to maximize the aerodynamic lift created by the lift-producing body or to minimize the drag induced by the lift-producing body.

Abstract: A system and method for detecting and compensating for thermal drift in an optical network in a manner that enables an increased number of optical channels to be used on a given optical medium, such as on a single optical fiber. A pair of narrow band, closely spaced optical signals from an optical transmitter function as a “temperature probe” signal. The two narrow band signals are centered within one passband of a filter of an optical device, such as an optical router. When the two narrow band signals are transmitted back to an optical receiver via the router, the magnitudes of the two signals are compared and a determination can be made as to the magnitude and direction of thermal drift of the passbands of the filter of the optical router.

Abstract: Apparatus and systems described herein provide for a randomly-accessible electrical busbar with a protective cover and an associated mating connector. Both the busbar and the associated mating connector have multiple, electrically conductive bristles protruding from a surface. The busbar is protected by a nonconductive fabric cover to reduce the risk of a person from accidentally contacting the electrically conductive bristles. A connection is made between the mating connector and the busbar by the bristles of the mating connector penetrating the protective fabric cover and interdigitating with the bristles of the busbar.