The present invention relates to a director mount arrangement for automatic alignment of a subsystem relative to a platform, wherein said director mount arrangement is arranged to pivotably support the subsystem. The director mount arrangement comprises a pivot frame arrangement and a control system. The control system comprises a control unit arranged to generate control signals so as to control the orientation of and stabilize the subsystem. The control signals are generated based on angular rate of subsystem and orientation operating commands provided from an operator. The control unit further generates estimated control signals based on platform orientation information and determine a difference between the control signals and the estimated control signals, wherein the difference is indicative of mechanical misalignments between the subsystem and the platform. The control unit further generates alignment corrections based on the determined difference so as to automatically align the subsystem relative to the platform.

The present invention relates to a director mount arrangement for automatic alignment of a subsystem relative to a platform, wherein said director mount arrangement is arranged to pivotably support the subsystem. The director mount arrangement comprises a pivot frame arrangement and a control system. The control system comprises a control unit arranged to generate control signals so as to control the orientation of and stabilize the subsystem. The control signals are generated based on angular rate of subsystem and orientation operating commands provided from an operator. The control unit further generates estimated control signals based on platform orientation information and determine a difference between the control signals and the estimated control signals, wherein the difference is indicative of mechanical misalignments between the subsystem and the platform. The control unit further generates alignment corrections based on the determined difference so as to automatically align the subsystem relative to the platform.

Several examples of a dual remote control and crew-served weapon station are described herein that uniquely provide different operating modes, any one of which can be quickly and efficiently selected based on outputs from various system sensors (e.g., switches and buttons). For example, a first operating mode is a mode in which the weapon is remotely steered and fired (e.g., remote controlled). A second operating mode is a mode in which a weapon cradle is stabilized by a gimbal and the weapon is aimed and fired by a local operator (e.g., crew-served stabilized). A third operating mode is a mode in which the cradle is manually steered and the weapon is fired by the local operator (e.g., full manual).

An aiming method for a weapon system including a weapon secured to a chassis, as well as an aiming device implementing such a method. The weapon system includes a computer having in an internal memory a nominal firing profile defined by the extreme elevation and relative bearing aiming instructions that are possible for the weapon, in the reference frame associated with the chassis, when the latter is in a firing position on a horizontal ground. The boundaries of the nominal firing profile are converted so as to determine a transformed firing profile which is delimited by the extreme directions of fire that are possible in the reference frame of the chassis when the latter is in the firing position on the field, and finally the operating firing profile is determined for the aiming, which is defined as the geometric intersection of the nominal firing profile and the transformed firing profile.

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.

An aiming method for a weapon system including a weapon secured to a chassis, as well as an aiming device implementing such a method. The weapon system includes a computer having in an internal memory a nominal firing profile defined by the extreme elevation and relative bearing aiming instructions that are possible for the weapon, in the reference frame associated with the chassis, when the latter is in a firing position on a horizontal ground. The boundaries of the nominal firing profile are converted so as to determine a transformed firing profile which is delimited by the extreme directions of fire that are possible in the reference frame of the chassis when the latter is in the firing position on the field, and finally the operating firing profile is determined for the aiming, which is defined as the geometric intersection of the nominal firing profile and the transformed firing profile.

An operating device and method for remotely controlling an arming device. The method includes confirming a tracking image at each firing time point of a laser beam transmitted by the range finder; based on an image correlation value of a target locked on by a tracking gate in the tracking image exceeding a threshold value, determining that the target is normally locked on; determining whether the laser beam from the range finder hits the target determined as being normally locked on based on a center value of the tracking image and a center value of the tracking gate; and based on the laser beam from the range finder hitting the target normally locked on, determining a range measurement value measured by the range finder as a true value of the target and determining other range measurement values as wrong measurement values.

Several examples of a dual remote control and crew-served weapon station are described herein that uniquely provide at least three operating modes, any one of which can be quickly and efficiently selected based on outputs from various system sensors (e.g., switches and buttons). For example, the first operating mode is a mode in which the weapon is remotely steered and fired (e.g., remote controlled). The second operating mode is a mode in which a weapon cradle is stabilized by a gimbal and the weapon is aimed and fired by a local operator (e.g., crew-served stabilized). The third operating mode is a mode in which the cradle is manually steered and the weapon is fired by the local operator (e.g., full manual).

The present invention relates to a director mount arrangement for automatic alignment of a subsystem relative to a platform, wherein said director mount arrangement is arranged to pivotably support the subsystem. The director mount arrangement comprises a pivot frame arrangement and a control system. The control system comprises a control unit arranged to generate control signals so as to control the orientation of and stabilize the subsystem. The control signals are generated based on angular rate of subsystem and orientation operating commands provided from an operator. The control unit further generates estimated control signals based on platform orientation information and determine a difference between the control signals and the estimated control signals, wherein the difference is indicative of mechanical misalignments between the subsystem and the platform. The control unit further generates alignment corrections based on the determined difference so as to automatically align the subsystem relative to the platform.