A system is described. The system may detect whether a user within a flight deck is authorized to control the aircraft. The user may receive differing levels of authority to control the aircraft depending on whether the user is authorized or unauthorized. The system may also control the aircraft depending on the various phases of the aircraft, including in flight and on the ground. The system may also be used to unlock the controls for the aircraft. The system may unlock the control using biometric information or nonbiometric information. The system may include a camera which is added to a flight deck. The camera may capture images of users within the flight deck. Faces within the images may be detected and compared against authorized users for locking or unlocking the aircraft controls.

An aircraft emergency control system comprises at least one sensor configured to output an electronic signal relating to detection of incapacitation of at least one aircraft crew member. A processor is configured to receive and process the electronic signal to determine whether emergency action is to be taken. A control unit is configured to communicate, in use, a control signal to an avionics system of the aircraft in relation to the emergency action if the processor determines that emergency action is to be taken.

Provided is an aerial vehicle including an emergency control device through power regulation. The aerial vehicle includes a power unit configured to supply power for the aerial vehicle, a flight control device configured to receive a wireless control signal from control terminal, and control a movement of the aerial vehicle based on the received control signal, and a power regulation device arranged between the power unit and the flight control device and configured to transmit the power from the power unit to the flight control device, wherein the power regulation device includes a communication unit configured to externally receive an emergency control signal through certain radio waves, a verification unit configured to verify whether the received emergency control signal is given according to a predetermined authority, and a power regulation unit configured to cut off the power supplied from the power unit to the flight control device.

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 monitoring terminal includes a transceiver, a receiver, and a processor. The transceiver provides a two-way communication with an unmanned aerial vehicle (UAV) via a first communication link and is configured to receive feedback data and a feedback data indication from the UAV and transmit control data to the UAV. The receiver is configured to receive the control data and a control data indication from a controlling terminal via a second communication link. The second communication link does not interfere with the first communication link. The processor is configured to determine whether the feedback data and the control data are being simultaneously transmitted via the first communication link based on the feedback data indication and the control data indication.

An unmanned aerial vehicle (UAV) flying method for helping an UAV flying to a location of an owner of the UAV or flying to a predetermined place includes the following steps of: triggering the UAV into a hijacked mode; ascertaining if the UAV is capable of flying or not; the UAV flying to the location of the owner or to the predetermined place if the UAV is capable of flying; and, the UAV sending a distress signal to the owner if the UAV is not capable of flying. Therefore, the UAV is capable of flying back or sending information after entering the hijacked mode, so as to avoid or lower the loss caused by losing the UAV or the UAV being captured by the captor.

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.

A device includes a transceiver, a receiver, and a processor. The transceiver is configured to receive feedback data from an unmanned aerial vehicle (UAV) and transmit control data to the UAV via a first communication link. The receiver is configured to receive the control data from a controlling terminal via a second communication link. The second communication link does not interfere with the first communication link. The processor is configured to determine whether the feedback data and the control data are being simultaneously transmitted via the first communication link.

Embodiments of the present invention relate to a method for generating search information of an unmanned aerial vehicle (UAV) and a UAV. The method includes: controlling a gimbal camera apparatus of the UAV to perform surround shooting to obtain character image information when the UAV is in an input locked state; matching the character image information with internal image information of the UAV; and generating the search information of the UAV according to a matching result. Therefore, a user can find the UAV in time according to the search information. In this way, theft is prevented, reducing the user loss.

Systems for policing and managing the operation of so-called unmanned vehicles are presented which allow for the takeover of the unmanned vehicle in the event of the detection of possible or actual ill-intentioned or inappropriate use of, malfunction or usurpation of the vehicle. Embodiments of the invention include dual-control unmanned vehicles which allow both pilot and police control of the vehicle, with the police having priority.