5 results about "Ballistics" patented technology

This invention relates to the field of unmanned aerial vehicle (UAV) automatic control technology, specifically to an UAV automatic window-breaking fire extinguishing system and method. The system uses an airborne lidar and image sensor to accurately measure the distance to the building wall and the target position, while simultaneously using a wind speed sensor to collect wind field data in real time. The control system is based on a ballistic model to comprehensively calculate the launch elevation angle, wind speed compensation, and recoil effects, dynamically adjusts the launch parameters of the fire extinguishing projectile, and uses a buffer mechanism to offset the launch impact, ensuring flight stability.

Provided herein are systems and methods that support preferred outcomes of tactical encounters. More particularly, the invention relates to artificial intelligence and machine learning systems and methods to select preferred ballistics solutions and tactical courses of action.

Improvements in a ballistic with a multi-part chamber locking assembly is disclosed to allow the casing ejection and reloading sequence to be temporarily slowed down to capture the optimum amount of ignited gun powders expanding gas, prior to the round exiting the barrel. Large slide component(s) of a firearm are replaced with a multi-part chamber locking assembly. This negates the requirement for a round to move laterally after moving vertically. The round only moves vertically thus mitigating the requirement for any forward motion. The multi-part chamber reduces the weight and materials needed to actuate all components of the ejecting and reloading process, so more energy is available to transfer movement of casing ejecting. The round is fired with a hammer or striker through impingement or a firing pin actuated action on a primer to ignite the propellant.

This invention discloses a method for designing the ballistic safety margin of a launch vehicle based on calibration test parameters, including: estimating the maximum safety margin x of the cluster stage. 01 ; in [0, x 01 Within the interval, values ​​are taken at equal intervals to obtain a set of safety margin values ​​for the cluster-binding stage; the reference ballistics corresponding to each safety margin value of the cluster-binding stage are obtained, and target simulation is performed based on the reference ballistics to determine the optimal value of the safety margin value of the cluster-binding stage; the maximum safety margin x of the second stage is estimated. 02 ; in [0, x 02 Within the specified interval, values ​​are taken at equal intervals to obtain a set of secondary safety margin values. Based on the optimal values ​​of the cluster-type launch vehicle safety margin obtained in step S3, the reference trajectory corresponding to each secondary safety margin value is obtained. Target simulation is performed based on the reference trajectory to determine the optimal values ​​of the secondary safety margins, and thus obtain the optimal values ​​of the tertiary safety margins. This invention enables the optimal allocation of safety margins at each stage of a cluster-type launch vehicle, maximizing its carrying capacity.

A system includes a shooting system comprising at least one first processor configured to: receive shooting ballistics-related data and shooting result data in real time; and detect real-time surrounding data; and an integrated computer comprising at least one second processor configured to: receive the shooting ballistics-related data and the shooting result data from the shooting system; derive learning result data based on the shooting ballistics-related data and the shooting result data; and transmit the learning result data to the shooting system.