Abstract: Autoland systems and processes for landing an aircraft without pilot intervention are described. In implementations, the autoland system includes a memory operable to store one or more modules and at least one processor coupled to the memory. The processor is operable to execute the one or more modules to identify a plurality of potential destinations for an aircraft. The processor can also calculate a merit for each potential destination identified, select a destination based upon the merit; receive terrain data and/or obstacle data, the including terrain characteristic(s) and/or obstacle characteristic(s); and create a route from a current position of the aircraft to an approach fix associated with the destination, the route accounting for the terrain characteristic(s) and/or obstacle characteristic(s). The processor can also cause the aircraft to traverse the route, and cause the aircraft to land at the destination without requiring pilot intervention.

Abstract: An Automatic Dependent Surveillance-Broadcast (ADS-B) avionics device for use in an aircraft with a transponder and an antenna comprises a first port, a second port, a transmitter, a switch, and a processing element. The first port may electrically couple to the transponder, and the second port may electrically couple to the antenna. The transmitter generates data to be transmitted over the antenna. The switch includes a first mode in which the transponder is electrically coupled to the antenna and a second mode in which the transmitter is electrically coupled to the antenna. The processing element is programmed to switch the switch from the first mode to the second mode, instruct the transmitter to transmit an ADS-B Out data packet to the second port, and switch the switch from the second mode to the first mode after the packet is transmitted.

Abstract: An obstacle avoidance system is provided to assist a pilot in avoiding obstacles. The obstacle avoidance system includes a set of proximity sensors and a pilot interface device. The set of proximity sensors detects nearby obstacles by emitting a signal and receiving a reflected signal from an obstacle. A processor receives an obstacle indication from the set of proximity sensors and detects the obstacle that is in proximity to the aircraft based at least in part on the reflected signal. The processor acquires a distance and a direction to the obstacle and calculates a threat level posed by the obstacle. The pilot interface device is operable to display the following: an ownship icon indicative of the aircraft, a velocity vector icon indicative of a velocity vector of the aircraft, and an obstacle graphic indicative of the distance, direction, and threat level of the obstacle.

Abstract: An improved integrated avionics system having a plurality of line replacement units (LRUs) is disclosed. At least one LRU stores in its memory software and configuration data stored and used by another LRU in the system. Upon detecting a new LRU installation, the at least one LRU may be configured to copy to its internal memory the software and configuration data loaded to the new LRU. The LRU may also store a table in its internal memory identifying each LRU that has been installed in the system, when each LRU was installed, and a copy of configuration and software data loaded to each LRU. If one of the LRUs in the system needs to be replaced, the LRU may determine which software and configuration data is applicable to the replaced LRU and load the determined software and configuration data to the new LRU, thereby improving the loading and installation process.

Abstract: An antenna array for use with an X-band weather radar system comprises a printed circuit board, a plurality of antenna elements, and a plurality of integrated circuit packages. The printed circuit board includes a first side and an opposing second side. The antenna elements are configured to transmit and receive radio waves at frequencies in the X-band. The antenna elements are electrically connected to the first side of the printed circuit board and positioned thereon in a two-dimensional array. A center of each antenna element is located on a point of a grid with grid points orthogonally spaced apart. Each integrated circuit package includes a transmitter electronic circuit and a receiver electronic circuit that are each in electronic communication with one antenna element. Each integrated circuit package is positioned on the first side of the printed circuit board to underlie one antenna element.

Abstract: A system for managing a communications log of audio data transmissions received and/or transmitted by an ownship aircraft includes a display screen, a memory operable to store audio signals and data associated with audio data transmissions, and a processor coupled to the display screen and to the memory. The processor determines the transmission frequency and time of receiving each received audio data transmission and creates a plurality of discrete display messages that include text identifying the determined frequency and time of receiving each received audio data transmission. The processor causes the discrete display messages to be displayed on the display, where they are selectable for playback by a user. Once selected, the processor generates an audio reproduction of the stored audio signals associated with the selected discrete display messages.

Abstract: An aircraft traffic system is provided that includes a primary antenna operable to generate interrogation signals and receive interrogation replies from other aircraft. The system additionally includes a secondary antenna configured as a tuned absorber having a matched impedance to at least partially absorb reflections of the interrogation signals or interrogation replies utilized by the primary antenna.

Abstract: Techniques are described that allow an air traffic display of an aircraft to display the relative motion of air traffic proximate to the aircraft. The air traffic display may be switched between a first display mode in which absolute motion of air traffic is displayed (e.g., motion of air traffic targets relative to a fixed point on the earth's surface or relative to an apparently fixed celestial point is displayed) and a second display mode in which motion of air traffic targets is displayed relative to the aircraft. The techniques further facilitate the selection of individual traffic targets from a displayed traffic depiction to activate a third display mode in which additional information about the relative motion of the selected target, such as its estimated closest point of approach (CPA) to the aircraft and the estimated time it will take the selected target to reach the CPA are shown.

Abstract: Techniques and systems are described that allow an air traffic display and/or avionics system of an aircraft to display and/or warn a pilot of aircraft targets for air traffic proximate to the aircraft or to suppress the display of on-ground air traffic targets. In some implementations, an integrated avionics system can use indirect information to determine whether an individual aircraft traffic target is to be presented to a pilot. For example, the integrated avionics system can determine whether an aircraft target is in proximity to the ground based on traffic tracking data corresponding to other aircraft.

Abstract: An aircraft radio comprises a receiver, an audio output, and a processing element. The receiver is tuned to a first radio frequency which provides a first audio signal and a second radio frequency which provides a second audio signal. The audio output provides an audio signal to a listening device. The processing element is coupled to a memory element and is configured to tune the receiver to the first radio frequency for a first time period, present the first audio signal to the audio output during the first time period, tune the receiver to the second radio frequency for a second time period to detect presence of the second audio signal, and present audio derived from the first audio signal to the audio output during at least a portion of the second time period.

Abstract: A touchscreen system for adapting a user interface broadly comprises a controller and a display screen, the display screen comprising a touchscreen. The display screen is operable to present the user interface. The controller may be configured to detect a defect in an area of the touchscreen, determine a location on the display screen related to the defect, and adapting the user interface on the display screen to compensate for the defect.

Abstract: An electronically steered weather radar system comprises a plurality of transmit/receive modules, a plurality of antenna modules, and a system signal processor. Each transmit/receive module may be configured to adjust a phase characteristic of a radio frequency (RF) signal to be transmitted and received. Antenna modules may be in communication with transmit/receive modules and may form an antenna array configured to transmit a system beam in a direction determined by the phase of the RF signal from each transmit/receive module and to generate the RF signal from the received system beam. The system signal processor may be configured to perform a first scan to detect meteorological formations wherein the system signal processor communicates with each transmit/receive module to adjust a phase characteristic of the RF signals such that the antenna array transmits and receives the system beam through a plurality of azimuth angles and a plurality of elevation angles.

Abstract: Techniques are described to simplify operation and maintenance of an aircraft by configuring an avionics unit to wirelessly communicate and receive avionics related data in a seamless fashion. In embodiments, an aircraft is equipped with a regulatory-certified avionics device configured to be installed in the aircraft. The system includes a memory card reader and associated memory card. The memory card includes a wireless transceiver to facilitate communication between the avionics unit and a mobile device (e.g., a tablet computer or smart phone employing a suitable application, a portable avionic device, etc.).

Abstract: A touchscreen system for adapting a user interface broadly comprises a controller and a display screen, the display screen comprising a touchscreen. The display screen is operable to present the user interface. The controller may be configured to detect a defect in an area of the touchscreen, determine a location on the display screen related to the defect, and adapting the user interface on the display screen to compensate for the defect.

Abstract: An aircraft audio panel includes a plurality of audio inputs each configured for receiving audio communications from an audio source; a plurality of audio outputs each configured for outputting the audio communications to audio equipment in the aircraft; selecting circuitry for selecting the audio communications between the audio inputs and the audio outputs; a single selector for permitting selection of one of the audio inputs or audio outputs for adjustment; and a single audio controller for permitting adjustment of an audio characteristic of the selected audio input or audio output. The audio panel may also include an audio characteristic indicator for indicating an audio characteristic of the selected audio input or audio output. The selecting circuitry may also implement a routing mode in which a user may first initiate the routing mode, then select one of the audio inputs for routing, and then select any one of the audio outputs for receiving audio communications from the selected audio input.

Abstract: Techniques are described that allow a system, such as a portable ADS-B-enabled device, to automatically determine whether the aircraft in which the system is employed is included in air traffic information (e.g., TIS-B air traffic information) broadcast by an air traffic control (ATC) ground station. The system includes a receiver assembly to receive a first transmission from a transponder of the aircraft that includes an identification address (e.g., an ICAO address) that identifies the aircraft. The receiver assembly also receives a second transmission from the ATC ground station that includes air traffic information and a client list including identification addresses of aircraft included in the air traffic information. The identification address of the aircraft is retrieved from the first transmission and used to determine whether the aircraft is included in the air traffic information by comparing the identification address with the identification addresses in the client list.

Abstract: An electronically steered weather radar system comprises a plurality of transmit/receive modules, a plurality of antenna modules, and a system signal processor. Each transmit/receive module may be configured to adjust the phase of a radio frequency (RF) signal to be transmitted and received. Each antenna module may be in communication with one transmit/receive module. The antenna modules may form an antenna array configured to transmit a system beam in a direction determined by the phase of the RF signal from each transmit/receive module and to generate the RF signal from the received system beam. The system signal processor may be configured to perform a first scan to detect meteorological formations wherein the system signal processor communicates with each transmit/receive module to adjust the phase of the RF signals such that the antenna array transmits and receives the system beam through a plurality of azimuth angles and a plurality of elevation angles.

Abstract: An electronic device is described that includes a range indicator for conveying a range of travel until the electronic device ceases operation due to loss of power. In implementations, the electronic device includes a display device, a memory operable to store one or more modules, and at least one processor coupled to the display device and the memory. The processor is operable to execute the one or more modules to cause display of navigation information at the display device. The navigation information includes a map graphic representing an area an aircraft is traversing. The navigation information also includes an end of use situation that represents a range of travel for the aircraft until the electronic device ceases operation due to a loss of power.

Abstract: Techniques and systems are described that allow an air traffic display and/or avionics system of an aircraft to display and/or warn a pilot of aircraft targets for air traffic proximate to the aircraft or to suppress the display of on-ground air traffic targets. In some implementations, an integrated avionics system can use indirect information to determine whether an individual aircraft traffic target is to be presented to a pilot. For example, the integrated avionics system can determine whether an aircraft target is in proximity to the ground based on traffic tracking data corresponding to other aircraft.

Abstract: A method for determining a height above ground of an aircraft broadly comprises the steps of generating a transmit signal with a transmitter, transmitting the transmit signal with a first antenna, generating a local oscillator signal with a local oscillator, receiving a receive signal with a second antenna, mixing the receive signal with the local oscillator signal to generate a baseband signal, determining a frequency of interest of the baseband signal, and calculating an aircraft altitude corresponding to the frequency of interest.