Abstract: A vertical landing vehicle including an airframe forming a hull and having at least one wing coupled to the airframe, at least one proximity sensor coupled to the airframe, and a flight control system including a control processor and an operator interface, wherein the at least one proximity sensor is coupled to the control processor, wherein the control processor, based on signals from the at least one proximity sensor, is configured to generate, for presentation through the operator interface, situational awareness indications corresponding to portions of the hull sensed by the at least one proximity sensor and obstacles sensed by the at least one proximity sensor, and wherein the situational awareness indications comprise a terrain map overlay including positional relationships between the hull and the obstacles.

Abstract: A vertical landing vehicle including an airframe forming a hull and having at least one wing coupled to the airframe, at least one proximity sensor coupled to the airframe, and a flight control system including a control processor and an operator interface, wherein the at least one proximity sensor is coupled to the control processor, wherein the control processor, based on signals from the at least one proximity sensor, is configured to generate, for presentation through the operator interface, situational awareness indications corresponding to portions of the hull sensed by the at least one proximity sensor and obstacles sensed by the at least one proximity sensor, and wherein the situational awareness indications comprise a terrain map overlay including positional relationships between the hull and the obstacles.

Abstract: A vertical landing vehicle including an airframe forming a hull and having at least one wing coupled to the airframe, at least one proximity sensor coupled to the airframe, and a flight control system including a control processor and an operator interface, the at least one proximity sensor being coupled to the control processor, the control processor being configured to receive proximity signals from the at least one proximity sensor and present, through the operator interface and based on the proximity signals, situational awareness information of obstacles within a predetermined distance of the vertical landing vehicle relative to the hull and/or the at least one wing.

Abstract: A vertical landing vehicle including an airframe forming a hull and having at least one wing coupled to the airframe, at least one proximity sensor coupled to the airframe, and a flight control system including a control processor and an operator interface, the at least one proximity sensor being coupled to the control processor, the control processor being configured to receive proximity signals from the at least one proximity sensor and present, through the operator interface and based on the proximity signals, situational awareness information of obstacles within a predetermined distance of the vertical landing vehicle relative to the hull and/or the at least one wing.

Abstract: Methods and apparatus for detecting surface deformation of aircraft surfaces are disclosed. An example apparatus includes a sensor system to monitor an aircraft surface, the sensor system including a first sensor and a second sensor. A surface monitoring system receives signals from the first sensor and the second sensor and based on the signals received, the surface monitoring system is to: detect a surface deformation on the aircraft surface; analyze one or more environmental conditions or aircraft parameters; and classify a severity of a detected surface deformation based on the one or more environmental conditions or aircraft parameters to determine if the detected surface deformation impacts aircraft performance or safety.

Abstract: A latency measurement system includes an event generation device that generates an initial event used to measure system latency. A component test system receives the event and in response outputs a test component output signal and a zero-latency indicator. An electronics system including a multifunction display unit receives the test component output signal and displays a visible element on the multifunction display unit. A camera generates a series of recorded images, where each recorded image contains an image of the zero-latency indicator and an image of the visible element. A processor then determines the system latency by determining a time difference in the series of recorded images between a representation of an occurrence of the event in the image of the zero-latency indicator and a representation of the occurrence of the event in the image of the visible element.

Abstract: A method and apparatus for managing communications. In one illustrative embodiment, an apparatus comprises a communications interface, an avionics interface, and a communications manager. The communications interface is configured to be connected to a group of wireless communications units. The avionics interface is configured to be connected to an avionics system. The communications manager is configured to identify the group of wireless communications units connected to the communications interface, receive input for a communications operation from a user interface in the avionics system, identify a number of wireless communications units in the group of wireless communications units for the communications operation from the input, and control operation of the number of wireless communications units to perform the communications operation.

Abstract: The present disclosure is directed to a system for, and method operating latency measurement including an event generation device that generates an initial event used to measure system latency. A component test system receives the event and in response outputs a test component output signal and a zero-latency indicator. An electronics system including a multifunction display unit receives the test component output signal and displays a visible element on the multifunction display unit. A camera generates a series of recorded images, where each recorded image contains an image of the zero-latency indicator and an image of the visible element. A processor then determines the system latency by determining a time difference in the series of recorded images between a representation of an occurrence of the event in the image of the zero-latency indicator and a representation of the occurrence of the event in the image of the visible element.

Abstract: Methods and systems for use in locating and prioritizing cargo are provided. The system includes a communications unit configured to receive location information and content information for each of a plurality of pieces of cargo from a cargo location and classification sensor (CLCS). The system also includes a cargo pickup planner module configured to determine a priority listing of pieces of cargo based on mission information, the location information, and the content information. The system also includes a cargo approach planner module configured to transmit a set of waypoints for specified pieces of cargo selected from the priority listing to a control system (FCS) configured to maneuver a vehicle to a position above a specified piece of cargo. The system further includes a cargo pickup overlay generator module configured to generate an overlay for a pilotage system (PS) display to assist a user in maneuvering the vehicle above each piece of cargo for pickup.

Abstract: Methods and systems for use in locating and prioritizing cargo are provided. The system includes a communications unit configured to receive location information and content information for each of a plurality of pieces of cargo from a cargo location and classification sensor (CLCS). The system also includes a cargo pickup planner module configured to determine a priority listing of pieces of cargo based on mission information, the location information, and the content information. The system also includes a cargo approach planner module configured to transmit a set of waypoints for specified pieces of cargo selected from the priority listing to a control system (FCS) configured to maneuver a vehicle to a position above a specified piece of cargo. The system further includes a cargo pickup overlay generator module configured to generate an overlay for a pilotage system (PS) display to assist a user in maneuvering the vehicle above each piece of cargo for pickup.

Abstract: The present disclosure is generally directed to a system for, and method operating a latency measurement system including an event generation device that generates an initial event used to measure system latency. A component test system receives the event and in response outputs a test component output signal and a zero-latency indicator. An electronics system including a multifunction display unit receives the test component output signal and displays a visible element on the multifunction display unit. A camera generates a series of recorded images, where each recorded image contains an image of the zero-latency indicator and an image of the visible element. A processor then determines the system latency by determining a time difference in the series of recorded images between a representation of an occurrence of the event in the image of the zero-latency indicator and a representation of the occurrence of the event in the image of the visible element.