Architectures and techniques are presented that can mitigate danger presented by an unsafe condition that can affect a vehicle or an occupant of the vehicle. An unsafe condition can be identified based on activation input, which can be received from an incident activation device such as a panic button or a sensor that detects the unsafe condition. The activation input can trigger an incident mitigation procedure that can determine a safe destination for the vehicle or occupant and a safe course by which to navigate to the safe destination.

In some embodiments, a control manager is disposed between the rotor system and the flight control inceptor. The control manager is configured to receive control commands wirelessly from a ground control station, translate the control commands into one or more axes associated with the flight control inceptor, and transmit the translated control commands to the rotor system in place of the instructions received from the pilot via the flight control inceptor.

Pilot health monitoring systems, methods, and apparatuses are provided. A pilot health monitoring system is configured to collect information regarding the pilot's physiological and/or physical characteristics, and information regarding a state of the aircraft; analyze the information; determine a health condition of the pilot and/or a state of the aircraft; and/or provide warnings and/or commands as a function of the information.

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.

In response to determining that a panic situation exists, an aircraft panic component can at least partially disable various systems of an aircraft, such as a navigation system (e.g., flight plans), an operational system (e.g., aircraft controls), or other suitable systems. For example, elements of a navigation and/or operational system of the aircraft may be disabled to disable local (e.g., pilot or cockpit) control of those system and/or to at least partially disable local operational systems of the aircraft (e.g., hydraulic or pneumatic flight control mechanisms, etc.). The navigation system can be updated with a new flight plan and the aircraft can have its autopilot engaged to pilot the aircraft according to the new flight plan such as to direct the aircraft to a certain altitude and/or heading. A remote terminal can be notified of the panic situation and control of the navigation system and/or operational systems can be turned over, potentially exclusively, to the remote terminal.

A method for policing and managing the operation of a flying, unmanned aircraft in the event of usurpation of control of, malfunction of, or ill-intentioned use of, this aircraft includes the steps of (a) detecting inappropriate operation of the aircraft; (b) transmitting a takeover command to the aircraft to interrupt control of the operation of this aircraft by a first pilot and relinquish control of the aircraft to a second pilot; and (c) transmitting control commands to the aircraft to control its operation by the second pilot, until the need for alternate pilot control of the aircraft has ended or until the aircraft has landed safely.

A system includes a first terminal configured to transmit control data to a controlled terminal via a first communication link for controlling operation of the controlled terminal, and a second terminal configured to transmit control data to the controlled terminal via a second communication link for controlling operation of the controlled terminal. The second terminal is further configured to, in response to the first communication link being under interference, receive the control data from the first terminal via a third communication link and transmit the control data received from the first terminal to the controlled terminal via the second communication link.

A navigation security module of an unmanned aerial vehicle (UAV) receives a combination of signals from a location technology, each signal comprising at least a signal identification and location data. The combination of signal identifications is processed against known identifications. If the identification is not found, or if the combination of signal identification is not possible, the signal may be a rogue signal, resulting in a quarantine protocol.

A technique for adaptively disrupting UAVs detects a target UAV using a camera, monitors the target UAV's communications using a directional antenna aligned with the camera, and attempts to communicate with the target UAV to request that it land, fly away, or return to launch. With the camera trained on the UAV, the directional antenna detects down-link signals from the UAV, which the UAV may employ to communicate with a ground-based controller. Control circuitry analyzes the down-link signals and generates a disrupting signal based thereon. The disrupting signal shares characteristics with the down-link signal, such as its protocol, bit rate, and/or packet length. The directional antenna transmits the disrupting signal back toward the UAV to affect the UAV's flight.

A method for policing and managing the operation of a flying, unmanned aircraft in the event of usurpation of control of, malfunction of, or ill-intentioned use of, this aircraft includes the steps of (a) detecting inappropriate operation of the aircraft; (b) transmitting a takeover command to the aircraft to interrupt control of the operation of this aircraft by a first pilot and relinquish control of the aircraft to a second pilot; and (c) transmitting control commands to the aircraft to control its operation by the second pilot, until the need for alternate pilot control of the aircraft has ended or until the aircraft has landed safely.