An submarine target device comprising an acoustic receiver, an acoustic transmitter and processing means adapted to perform a first cycle of operations comprising detecting within an acoustic stream captured by the acoustic receiver, the start of a first signal corresponding to characteristics of at least one acoustic transmitter remote from at least one detector; triggering the recording of the first signal; detecting, within the acoustic stream, the end of the first signal and triggering the cessation of recording; then a second cycle of operations comprising detecting, within the acoustic stream, the start of a second signal corresponding to said characteristics; and triggering the transmission of the first signal, via the acoustic transmitter.

The illustrative embodiments provide for a method a training system. The training system includes a physical sensor system connected to a physical vehicle. The physical sensor system is configured to obtain real atmospheric obscuration data of a real atmospheric obscuration. The training system also includes a data processing system comprising a processor and a tangible memory. The data processing system is configured to receive the real atmospheric obscuration data, and determine based on the real atmospheric obscuration data whether a target is visible to the physical vehicle in a simulation training environment generated by the data processing system. The simulation training environment at least including a virtual representation of the physical vehicle and a virtual representation of the real atmospheric obscuration.

The present invention relates to a training system for training of a forward controller. The training system utilizes a pod housing that can be attached to a hardpoint under an aircraft wing. The pod is configured to receive communications from the forward controller on the ground (or in another aircraft) and communicate wirelessly with an HMD and/or electronic device in the cockpit of the aircraft. This allows cheaper, less expensive aircraft to be used for training purposes.

A method for facilitating real time tracking of an airborne asset via downlink of GPS signals that are usable for determining asset location information from the asset to a ground station may include receiving a first GPS signal and a second GPS signal at a device disposed on the airborne asset and combining the first and second GPS signals to form combined signal responsive to filtration and amplification of the first and second GPS signals. The method may further include employing an overlay analog translation to convert the combined signal into a composite signal at a different frequency than the combined signal, generating a pilot carrier frequency for association with the composite signal, and amplifying the composite signal prior to transmission via the downlink from the airborne asset to the ground station. The pilot carrier frequency and amplitude may be adjustable.

An inflatable dummy target fittable into a carrier missile capable of being released from the carrier missile during exo-atmospheric flight; upon release, the dummy target or portion thereof is capable of being inflated and manifest characteristics that resemble GTG missile characteristics, wherein the GTG missile characteristics include IR signature, RF signature and GTG missile.

A dynamic infrared (IR) scene generation system comprising a thin-film screen configured to react to contact by an IR laser; a laser scanning system configured to contact the thin-film screen with laser beam, the laser scanning system comprising a laser scanner, one or more modulators, and an IR laser source; and an image processing system operably connected to a controller configured to control the laser scanning system based on data from the image processing system, wherein the laser scanning system can be configured to contact the thin-film screen with the IR laser based on an IR scene input.

Disclosed herein is a system and method for simulating real-time visualizable electronic warfare. The system includes a location calculation unit for calculating location coordinates of the aircraft and the missile for each frame according to a display frame rate, a display unit for visualizing, for each frame, movement of the aircraft and the missile depending on the location coordinates thereof, a precise tracking unit for, when a relative distance between the aircraft and the missile is less than a dangerous distance, dividing an interval between a current frame and a subsequent frame into sub-intervals based on the display frame rate, and sampling locations of the aircraft and the missile, and a proximity fuse control unit for processing the missile to explode when a relative distance between sampled locations of the aircraft and the missile, is less than or equal to a maximum explosible distance of a proximity fuse of the missile.

A method and apparatus is provided that provides accurate navigation for spin-stabilized projectiles in a GPS-denied environment using low cost measurement sensors, by application of flight dynamics in real-time state estimation algorithms.

An inflatable dummy target comprising a chassis of inflatable ducts wrapped with a sheet. The chassis of inflatable ducts can include one or more ring shaped ducts and one or more elongate ducts. The chassis can include at least two ring shaped ducts interconnected by one or more elongate ducts. The dummy target can include several attached axi-symmetrical sections, each section have a chassis of inflatable ducts. Each section can be conical, frustoconical or cylindrical, thereby achieving a concave or convex dummy target geometry.

A method for ascertaining position information for an effector after launching from a launcher of a weapons system including the effector and at least one weapons system unit different from the effector, includes receiving a time synchronization signal at the effector in such a way that the effector and the at least one weapons system unit are temporally synchronized at the latest when the effector is launched. The effector furthermore receives position data of the at least one weapons system unit and a timestamp with unique assignment to the position data through a wireless communication connection after the effector has been launched. Position information is ascertained based on the timestamp, the effector's own time upon receipt of the timestamp, and the position data assigned uniquely to the timestamp. An effector, a computing unit and a weapons system are also provided.