An integrated architecture and its associated sensors and processing software subsystems are defined and developed allowing a conventional unguided bullet to be transformed into a guided bullet without the use of an on-board inertial measurement unit (IMU). Some important SW components of the present disclosure include a target state estimator (TSE); a bullet state estimator (BSE); Multi-Object Tracking and Data Association; NTS GL; and a Data Link. Pre-conversion of two angles and range information of an OI sensor from spherical coordinates into Cartesian coordinates eliminates the Jacobian dependency in the H matrix for the BSE, thus increasing the miss distance performance accuracy of the bullet target engagement system.

An integrated architecture and its associated sensors and processing software subsystems are defined and developed allowing a conventional unguided bullet to be transformed into a guided bullet without the use of an on-board inertial measurement unit (IMU). Some important SW components of the present disclosure include a target state estimator (TSE); a bullet state estimator (BSE); Multi-Object Tracking and Data Association; NTS GL; and a Data Link. Pre-conversion of two angles and range information of an OI sensor from spherical coordinates into Cartesian coordinates eliminates the Jacobian dependency in the H matrix for the BSE, thus increasing the miss distance performance accuracy of the bullet target engagement system.

According to embodiments of the present disclosure, a multi-armament control system is provided. The multi-armament control system includes: platforms including an armament; and an operating vehicle configured to operate the platforms based on a single controller of the operating vehicle. The operating vehicle is further configured to acquire information about a target according to presence or absence of the target, generate a position of a directing point of the target, and share the position of the directing point of the target with the platforms. At least one from among the operating vehicle and the platforms is configured to construct fixed fire nets or variable fire nets of the platforms according to whether the target moves, and by, in part, assigning priority, to each of the platforms based on the target and the firing range of the armament of the platforms.

According to embodiments of the present disclosure, a multi-armament control system is provided. The multi-armament control system includes: platforms including an armament; and an operating vehicle configured to operate the platforms based on a single controller of the operating vehicle. The operating vehicle is further configured to acquire information about a target according to presence or absence of the target, generate a position of a directing point of the target, and share the position of the directing point of the target with the platforms. At least one from among the operating vehicle and the platforms is configured to construct fixed fire nets or variable fire nets of the platforms according to whether the target moves, and by, in part, assigning priority, to each of the platforms based on the target and the firing range of the armament of the platforms.

A flying vehicle is disclosed with a projectile module or component that contains a projectile for projecting at another flying device. The flying vehicle receives an identification of a target flying device and applies a projectile model which generates a determination that indicates whether a projectile, if fired from the projectile component, the projectile will hit the target flying device. The projectile model taking into account one or more of a wind modeling in an area around the flying vehicle based on an inference of wind due to a tilt of the flying vehicle, a projected path of the target device based on its identification and a drag on the projectile as it deploys from the projectile component. When the determination indicates that the projectile will hit the targeted device according to a threshold value, the flying vehicle fires the projectile at the targeted flying device.

A flying vehicle is disclosed with a projectile module or component that contains a projectile for projecting at another flying device. The flying vehicle receives an identification of a target flying device and applies a projectile model which generates a determination that indicates whether a projectile, if fired from the projectile component, the projectile will hit the target flying device. The projectile model taking into account one or more of a wind modeling in an area around the flying vehicle based on an inference of wind due to a tilt of the flying vehicle, a projected path of the target device based on its identification and a drag on the projectile as it deploys from the projectile component. When the determination indicates that the projectile will hit the targeted device according to a threshold value, the flying vehicle fires the projectile at the targeted flying device.

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.

A boresighting device to equip a turret provided with a barrel and one or several sight system(s) each with an optical system includes: a deflection target intended to be positioned outside the barrel, at a muzzle brake of the barrel; a housing intended to be positioned outside the barrel, at a shaft of the barrel. The housing includes: a first optics system provided with a deflection camera, the first optics system being used to determine a parallelism error between a firing line from the shaft and that from the muzzle brake; and a second optics system provided with a boresighting camera, the second optics system being used to determine a parallelism error between the firing line from the shaft and an optics line from the sight system(s). The deflection target integrates a geometric figure serving as a reference point for the first optics system.

A boresighting device to equip a turret provided with a barrel and one or several sight system(s) each with an optical system includes: a deflection target intended to be positioned outside the barrel, at a muzzle brake of the barrel; a housing intended to be positioned outside the barrel, at a shaft of the barrel. The housing includes: a first optics system provided with a deflection camera, the first optics system being used to determine a parallelism error between a firing line from the shaft and that from the muzzle brake; and a second optics system provided with a boresighting camera, the second optics system being used to determine a parallelism error between the firing line from the shaft and an optics line from the sight system(s). The deflection target integrates a geometric figure serving as a reference point for the first optics system.