Aircraft instrumentation systems and controllers are provided. An aircraft instrumentation system includes a display and a controller. The controller is configured to monitor an electronic circuit breaker (ECB) status of each of a plurality of aircraft systems. The controller is further configured to generate, for each of the plurality of aircraft systems, a visual indicator that indicates the ECB status. The controller is yet further configured to generate an image arrangement that includes the visual indicator for each of the plurality of aircraft systems and to generate a signal that causes a display to present the image arrangement.

Methods, systems, and apparatus, including computer programs encoded on computer storage media, for an unmanned aerial system inspection system. One of the methods is performed by a UAV and includes receiving, by the UAV, flight information describing a job to perform an inspection of a rooftop. A particular altitude is ascended to, and an inspection of the rooftop is performed including obtaining sensor information describing the rooftop. Location information identifying a damaged area of the rooftop is received. The damaged area of the rooftop is traveled to. An inspection of the damaged area of the rooftop is performed including obtaining detailed sensor information describing the damaged area. A safe landing location is traveled to.

In some embodiments, the present disclosure provides systems and methods enabling unmanned vehicle navigation and delivery including an integrated roofing accessory integrated into a roof, the integrated roofing accessory including at least one antenna and a computing module in communication with the at least one antenna, where the computing module, when software is executed, is configured to transmit, via the at least one antenna: electronic operating instructions to at least one unmanned vehicle, and network messages related to the at least one unmanned vehicle to at least one additional integrated roofing accessory. A landing member is on the roof and the electronic operating instructions comprise: at least one landing instruction configured to cause the at least one unmanned vehicle to land on the landing member, and at least one take-off instruction configured to cause the at least one unmanned vehicle to take off from the landing member.

A method for optimizing a climb phase of an aircraft, implemented repeatedly during the climb phase, includes an acquiring step for acquiring current values of input parameters, a determining step for determining a current optimized DT.sub.flex value from the current values of the input parameters and from optimized DT.sub.flex values recorded in a database and a transmitting step for transmitting the determined current optimized DT.sub.flex value to a user system with a view to controlling the thrust of the aircraft, the method making it possible to continuously adapt, during the climb phase, the optimized DT.sub.flex value so it corresponds to current conditions of the aircraft to maximize its performance particular for fuel consumption.

Present novel and non-trivial system, device, and method for generating a vertical path profile are disclosed. The vertical path profile generating system is comprised of a source of navigation data, a source of performance factors data, a vertical path generator (VPG) and a presentation system. The VPG may be configured to receive the navigation data representative of takeoff runway information; receive the performance data may be representative of aircraft performance factors; determine a first vertical path and/or second vertical path as a function of criteria employing the navigation data and the performance data; generate presentation data responsive to the determination; and provide the presentation data to one or more presentation devices comprised of, in part, a visual display unit configured to display a first takeoff path profile and/or a second takeoff path profile.

Embodiments herein describe a perch for screening drones before permitting access to a restricted geographic region. The perch may include various scanners for evaluating the payload of the drone, its hardware, and flight control software. In one embodiment, the screening perch includes a conveyor belt that moves the drone through various scanners or stages in the perch. In one embodiment, the perch ensures the drone is properly configured to enter the restricted geographic region. The region may include multiple requirements or criteria that must be satisfied before a drone is permitted to enter. For example, the drone may need a signed flight plan, cargo that is less than a certain percentage of its weight, or an approved flight controller before being permitted into the restricted region. In this manner, the perch serves as a controlled entrance point for drones attempting to enter the restricted region.

Flight deck display systems and methods for generating cockpit displays including dynamically-adjustable runway length symbology are provided. In one embodiment, the flight deck display system includes a display device to which a controller is operably coupled. A cockpit display, such as a primary fight display, is generated on the display device. The cockpit display is generated to include a runway graphic and a usable runway end marker. During operation of the display system, the controller receives runway usage restriction data identifying any currently restricted sections of a runway approached for usage by the aircraft. The controller further determines a dynamically-adjusted usable runway length as a function of the runway usage restriction data and then adjusts the position of the usable runway end marker, as generated on the cockpit display, along the length of the runway graphic in accordance with the dynamically-adjusted usable runway length.

Methods, systems, and computer readable media for managing aircraft radiofrequency communications on board an aircraft are disclosed. In some aspects, a method can include determining at least one communication frequency, the at least one communication frequency corresponding to a communication center within a radio horizon of the aircraft, displaying the at least one communication frequency at an interface, and where there is more than one communication frequency displayed on the interface: filtering the more than one communication frequency according to a flight step of the aircraft in order to reduce a number of the more than one communication frequency displayed on the interface, and sorting the more than one communication frequency according to occupation rate in order to prioritize the more than one communication frequency displayed on the interface, and thereby aid in predicting a communication frequency communicated to the aircraft.

Disclosed are examples of systems, apparatus, methods and computer program products for locating unmanned aerial vehicles (UAVs). A region of airspace may be scanned with two scanning apparatuses. Each scanning apparatus may include one or more directional Radio Frequency (RF) antennae. The two scanning apparatuses may have different locations. Radio frequency signals emitted by a UAV can be received at each of the two scanning apparatuses. The received radio frequency signals can be processed to determine a first location of the UAV.

Flight deck display systems and methods for generating cockpit displays including dynamically-adjustable runway length symbology are provided. In one embodiment, the flight deck display system includes a display device to which a controller is operably coupled. A cockpit display, such as a primary fight display, is generated on the display device. The cockpit display is generated to include a runway graphic and a usable runway end marker. During operation of the display system, the controller receives runway usage restriction data identifying any currently restricted sections of a runway approached for usage by the aircraft. The controller further determines a dynamically-adjusted usable runway length as a function of the runway usage restriction data and then adjusts the position of the usable runway end marker, as generated on the cockpit display, along the length of the runway graphic in accordance with the dynamically-adjusted usable runway length.