A system for aligning a weapon to a high-performance target sensor. A reference measurement sensor installed on the target sensor measures the direction and range to each of several references points on the weapon. From these measurements, and measurement by the target sensor of target states, a processing circuit calculates the states of the target in a coordinate system of the weapon. Each reference point may be a retroreflector; the reference measurement sensor may include an imaging sensor to measure direction, and a laser range finder to measure range.

A system for aligning a weapon to a high-performance target sensor. A reference measurement sensor installed on the target sensor measures the direction and range to each of several references points on the weapon. From these measurements, and measurement by the target sensor of target states, a processing circuit calculates the states of the target in a coordinate system of the weapon. Each reference point may be a retroreflector; the reference measurement sensor may include an imaging sensor to measure direction, and a laser range finder to measure range.

A target location device has a video camera, a range finder, a self location module and an inertial measurement unit. The device provides a video display including video output of the camera and an object marker such as a cross-hair overlayed on the video output for aiming the camera on a reference point or on a target in the video output. The range finder determines a distance from the device to the target. The self location module identifies the geographic location of the device. The inertial measurement unit includes at least one gyro for providing outputs corresponding to the location of the reference point and the target. Video stabilization may be use to allow accurate placement of the object marker on the target or reference point. Automatic range finder firing and gyroscope error compensation are also provided.

A light irradiation device includes: at least one imaging means that images a monitoring region to continue to accurately irradiate a moving target with light; at least one projection means that irradiates the monitoring region with signal light; a control means that controls the imaging means to image the monitoring region and controls the projection means to emit the signal light; at least one propeller that moves the own device in the air; and a flight control means that controls flight of the own device by controlling the propeller, the control means controlling, when recognizing a light irradiation target to be irradiated with the signal light on image data imaged by the imaging means, the projection means to emit the signal light toward the light irradiation target.

A remote weapon system structured to be interfaced with aerial, ground and sea vehicles or platforms for operation in mission critical conditions, allows for mounting and control of single or multi-shot anti-armor rocket launcher systems and provides optical sighting, laser range finding and fire control to adjust vertical elevation, sight of target and trigger of the ignition system. A tactical gimbal controlled by a high torque motor with dual shafts allows for high positional accuracy and target hold that is stable. A frame shrouds and secures rocket launcher tubes causing them to move in unison with the tactical gimbal as a single or multi-shot system. Ignition of the rocket(s) is achieved by a remote-controlled ignitor.

A remote weapon system structured to be interfaced with aerial, ground and sea vehicles or platforms for operation in mission critical conditions, allows for mounting and control of single or multi-shot anti-armor rocket launcher systems and provides optical sighting, laser range finding and fire control to adjust vertical elevation, sight of target and trigger of the ignition system. A tactical gimbal controlled by a high torque motor with dual shafts allows for high positional accuracy and target hold that is stable. A frame shrouds and secures rocket launcher tubes causing them to move in unison with the tactical gimbal as a single or multi-shot system. Ignition of the rocket(s) is achieved by a remote-controlled ignitor.

The neutralisation system (1) comprises a drone (2) configured to be able to fly close to a target and transmit at least position information concerning the position of the target, the neutralisation system (1) also comprising at least one missile (6) capable of being guided towards the target in order to neutralise it and at least one control station (8), the control station (8) comprising a receiving unit (9B) capable of receiving at least the position information transmitted by the drone (2) and a display unit (10A) capable of displaying this information to an operator, the missile (6) being configured to be able to be guided towards the target by means of the position information received by the control station (8).

The neutralisation system (1) comprises a drone (2) configured to be able to fly close to a target and transmit at least position information concerning the position of the target, the neutralisation system (1) also comprising at least one missile (6) capable of being guided towards the target in order to neutralise it and at least one control station (8), the control station (8) comprising a receiving unit (9B) capable of receiving at least the position information transmitted by the drone (2) and a display unit (10A) capable of displaying this information to an operator, the missile (6) being configured to be able to be guided towards the target by means of the position information received by the control station (8).

A remote weapon system structured to be interfaced with aerial, ground and sea vehicles or platforms for operation in mission critical conditions, allows for mounting and control of single or multi-shot anti-armor rocket launcher systems and provides optical sighting, laser range finding and fire control to adjust vertical elevation, sight of target and trigger of the ignition system. A tactical gimbal controlled by a high torque motor with dual shafts allows for high positional accuracy and target hold that is stable. A frame shrouds and secures rocket launcher tubes causing them to move in unison with the tactical gimbal as a single or multi-shot system. Ignition of the rocket(s) is achieved by a remote-controlled ignitor.

A remote weapon system structured to be interfaced with aerial, ground and sea vehicles or platforms for operation in mission critical conditions, allows for mounting and control of single or multi-shot anti-armor rocket launcher systems and provides optical sighting, laser range finding and fire control to adjust vertical elevation, sight of target and trigger of the ignition system. A tactical gimbal controlled by a high torque motor with dual shafts allows for high positional accuracy and target hold that is stable. A frame shrouds and secures rocket launcher tubes causing them to move in unison with the tactical gimbal as a single or multi-shot system. Ignition of the rocket(s) is achieved by a remote-controlled ignitor.