Methods and systems for providing alerts in an aircraft. The methods and systems receive a flight plan and conditions data providing information on flight conditions along the flight plan including meteorological data. The conditions data is analyzed in flying regions along the flight plan to determine flight rules information. An alert is output to flight crew of the aircraft. The alert predicts when and where a change between type of flight rules will occur based on the flight rules information.

A portable computerized device for an aircraft control system includes an input system for inputting commands, a device display for displaying information on the computerized device, a processor, a wireless communication module, and a non-transitory computer readable medium comprising computer executable instructions, the computer executable instructions configured to cause the processor to perform a method. The method can include detecting whether the portable computerized device is in a cockpit state such that the portable computerized device is in and/or docked to an aircraft cockpit or if the portable computerized device is in a remote state such that the portable computerized device is not in an aircraft cockpit or is not docked to an aircraft cockpit. If the portable computerized device is determined to be in a remote state, the method includes operating the remote device in a remote mode. If the portable computerized device is determined to be in a cockpit state, the method includes operating the device in a local mode.

Systems, methods, and devices are provided for controlling an unmanned aerial vehicle (UAV) associated with flight response measures. The flight response measure may be generated by assessing one or more flight-restriction strips, assessing at least one of a location or a movement characteristic of the UAV relative to the one or more flight-restriction strips, and directing, with aid of one or more processors, the UAV to take one or more flight response measures based on at least one of the location or movement characteristic of the UAV relative to the one or more flight-restriction strips.

A system for aircraft recommendation for an electric aircraft is presented. The system includes a computing device, wherein the computing device is configured to, receive an aircraft datum, receive a flight plan, generate a model of at least a flight phase as a function of the aircraft datum and the flight plan, generate an aircraft recommendation as a function of the flight plan and aircraft datum, wherein generating the aircraft recommendation further comprise identifying a tunable parameter of the at least a flight phase, tuning the tunable parameter as a function of the model of the at least a flight phase and at least an objective constraint, and generating the aircraft recommendation as a function of the tuning. The system further includes a user device, wherein the user device is configured to display the aircraft recommendation.

Disclosed are methods, systems, and non-transitory computer-readable medium for distributed vehicle processing. For instance, the method may include: in response to determining a first trigger condition of a first set of trigger conditions is satisfied, performing a first process corresponding to the first trigger condition on-board a vehicle; in response to determining a second trigger condition of a second set of trigger conditions is satisfied, prompting a second process corresponding to the second trigger condition by transmitting an edge request to an edge node and receiving an edge response from the edge node; and in response to determining a third trigger condition of a third set of trigger conditions is satisfied, prompting a third process corresponding to the third trigger condition by transmitting a cloud request to a cloud node and receiving a cloud response from the cloud node.

A system for providing air traffic control within a geographic sector to which a communication frequency in the VHF or UHF range is assigned comprises at least one satellite (configured for a communication with an aircraft in the geographic sector using an analog modulated RFF signal at the communication frequency. The system is configured in such a way that at each time, only one satellite is actively transmitting on the communication frequency assigned to the geographic sector.

A system for transmitting and storing data based on a connection for a vehicle is presented. The system includes a computing device, the computing device configured to receive a vehicle data, communicatively connect the computing device to a second device as a function of a mesh network, authenticate a second device as a function of an authentication module, generate a vehicle collection datum as a function of the vehicle data, communicate the vehicle collection datum to the second device as a function of the mesh network, and store the vehicle collection datum in a recorder database as a function of a lack of identification of the mesh network.

A system for flight tracking of an electric aircraft is presented. A system includes a non-volatile data storage unit. A non-volatile data storage unit is housed within a protective barrier of an electric aircraft. A non-volatile data storage unit is configured to receive flight data of an electric aircraft from a computing device. A non-volatile data storage unit is configured to record flight data. A non-volatile data storage unit is configured to categorize flight data to at least two flight data groups. A system includes a computing device. A computing device is housed within an electric aircraft. A computing device is configured to receive flight data from at least a sensor of an electric aircraft. A computing device is configured to convey flight data to a non-volatile data storage unit. A computing device is configured to transmit flight data to at least an external computing device.

Various avionics systems may benefit from repeaters. For example, an ADS-B In traffic display repeater system may be useful for, for example, retrofit aircraft. A system, according to certain embodiments, can include a traffic awareness computer of an aircraft. The system can also include an aircraft interface device. The system can further include a data bus configured to convey data from the traffic awareness computer to the aircraft interface device. The data conveyed can be configured to permit repetition of one or more displays of a cockpit of the aircraft on a tablet computer.

Systems and methods for airspace management. One embodiment of an aerial vehicle, includes a first sensor for detecting a lateral field of view of the aerial vehicle and a vehicle computing device. The vehicle computing device may include a memory component and a processor. The memory component may store logic that, when executed by the processor, causes the aerial vehicle to calculate a detection boundary for the aerial vehicle to maintain a well clear requirement, wherein the detection boundary is based on instantaneous trajectory, planned future trajectory, and a capability of the aerial vehicle and utilize the capability of the aerial vehicle and data from the first sensor to maintain the vehicle within detection boundary. In some embodiments the logic may cause the vehicle to provide an instruction to maintain the aerial vehicle within the detection boundary.