Abstract: A method for passive aerial cord release mechanisms and an aerial cord release mechanism for an aerial vehicle (AV). A method includes determining a retracting force to be applied to a winch of an aerial vehicle (AV), wherein the determined retracting force is a force required to retract a cord to be coiled around the winch within the AV, and the cord is temporarily coupled to the winch, such that an external force exceeding a predetermined threshold causes decoupling between the cord and the winch.

Abstract: A self-release mechanism. The self-release mechanism includes a counter-weight, wherein the counter-weight is located on a first end of the self-release mechanism; a shaft having a top portion and a bottom portion, wherein the top portion of the shaft is coupled to the counter-weight, wherein the shaft defines a perforation, wherein the perforation is adapted to receive a cord; and a hook including a hook bend, wherein the hook is located on a second end of the self-release mechanism, wherein the hook is coupled to the bottom portion of the shaft, wherein the self-release mechanism moves to a first position when a tension is exerted on the self-release mechanism due to gravity caused by coupling of the hook to a payload via the hook bend, wherein the self-release mechanism moves to a second position when the exerted tension is released.

Abstract: A method for passive aerial cord release mechanisms and an aerial cord release mechanism for an aerial vehicle (AV). A method includes determining a retracting force to be applied to a winch of an aerial vehicle (AV), wherein the determined retracting force is a force required to retract a cord to be coiled around the winch within the AV, and the cord is temporarily coupled to the winch, such that an external force exceeding a predetermined threshold causes decoupling between the cord and the winch.

Abstract: A self-release mechanism. The self-release mechanism includes a counter-weight, wherein the counter-weight is located on a first end of the self-release mechanism; a shaft having a top portion and a bottom portion, wherein the top portion of the shaft is coupled to the counter-weight, wherein the shaft defines a perforation, wherein the perforation is adapted to receive a cord; and a hook including a hook bend, wherein the hook is located on a second end of the self-release mechanism, wherein the hook is coupled to the bottom portion of the shaft, wherein the self-release mechanism moves to a first position when a tension is exerted on the self-release mechanism due to gravity caused by coupling of the hook to a payload via the hook bend, wherein the self-release mechanism moves to a second position when the exerted tension is released.

Abstract: Apparatus for capturing images while in motion, including at least one CCD camera housed within an aircraft traveling along a flight path, for capturing aerial images of ground terrain, a motor for rotating an axis on which the at least one CCD camera is mounted, and for generating a sweeping back-and-forth motion for a field of view of the at least one CCD camera, the sweeping motion being transverse to the aircraft flight path, and an optical assembly connected to said at least one CCD camera.

Abstract: A navigation termination system of an unmanned vehicle (UV) is provided. The system includes a plurality of sensors connected to the UV and configured to detect motion of the UV; a power supply configured to power the movement of the UV; a processing circuitry; and a memory, the memory containing instructions that, when executed by the processing circuitry, configure the system to: determine, based on sensory signals captured by the plurality of sensors, a navigation termination event; and disrupt a connection between the power supply and a motion mechanism of the UV when the navigation termination event occurs.

Abstract: Apparatus for capturing images while in motion, including at least one CCD camera housed within an aircraft traveling along a flight path, for capturing aerial images of ground terrain, a motor for rotating an axis on which the at least one CCD camera is mounted, and for generating a sweeping back-and-forth motion for a field of view of the at least one CCD camera, the sweeping motion being transverse to the aircraft flight path, and an optical assembly connected to said at least one CCD camera.