A method of executing a mission for at least one mobile munition assembly in a mission environment is provided, the at least one mobile munition assembly having a container that encloses one or more launchers configured to receive and launch a munition. One or more electronic devices in communicatively coupling with one another in the mission environment form a secure network. A status of a situational awareness (SA) corresponding to each of the one or more electronic devices in the mission environment is transmitted. An input of parameters of the mission for the at least one mobile munition assembly is enabled, the parameters having one or more predefined rules associated therewith and configured to be applied to the parameters based on at least the status of the situational awareness (SA). An authorization or a denial of the mission for the at least one mobile munition assembly is requested.

A winged external guidance frame placed on the muzzle that can couple with a projectile while exiting the barrel utilizing the kinetic energy of the projectile to travel to the target while the accuracy is provided by on board electronics and corrected using the wings. Alternately a reusable unmanned aerial system that travels in the speed and direction of the projectile and couples with the projectile as it exits the barrel.

A method for authorizing a mission for at least one portable launch assembly in a defined hazard area is disclosed. One or more electronic devices may be communicatively coupled to one another. At least signals representative of a situational awareness (SA) corresponding to each of the one or more electronic devices, and parameters of the mission for the at least one portable launch assembly, may be received. One or more predefined rules may be selectively retrieved, and may be applied to the parameters of the mission based on at least the signals representative of a situational awareness (SA) corresponding to each of the one or more electronic devices. And, a request for an approval of the mission for the at least one portable launch assembly may be obtained, the request for the approval based on at least the one or more predefined rules related to the parameters of the mission.

A winged external guidance frame placed on the muzzle that can couple with a projectile while exiting the barrel utilizing the kinetic energy of the projectile to travel to the target while the accuracy is provided by on board electronics and corrected using the wings. Alternately a reusable unmanned aerial system that travels in the speed and direction of the projectile and couples with the projectile as it exits the barrel.

A method for determining a fire guidance solution of an artillery weapon in indirect ballistic fire to hit a target. A changing weapon position of the weapon and a target position of the target are taken into consideration as geographical position data.

A method for determining a fire guidance solution of an artillery weapon in indirect ballistic fire to hit a target. A changing weapon position of the weapon and a target position of the target are taken into consideration as geographical position data.

A winged external guidance frame placed on the muzzle that can couple with a projectile while exiting the barrel utilizing the kinetic energy of the projectile to travel to the target while the accuracy is provided by on board electronics and corrected using the wings. Alternately a reusable unmanned aerial system that travels in the speed and direction of the projectile and couples with the projectile as it exits the barrel.

Systems, devices, and methods for determining a predicted impact point of a selected weapon and associated round based on stored ballistic information, provided elevation data, provided azimuth data, and provided position data.

Systems, devices, and methods for determining a predicted impact point of a selected weapon and associated round based on stored ballistic information, provided elevation data, provided azimuth data, and provided position data.

Systems, devices, and methods for determining a predicted impact point of a selected weapon and associated round based on stored ballistic information, provided elevation data, provided azimuth data, and provided position data.