Software is provided for functioning in conjunction with a plurality of mission stores and for assisting a pilot of a vehicle with release of the mission stores to achieve a specified number of mission objectives. Each of the plurality of mission stores may be designated for communication with a separate mission reference point or target. The targets may be grouped within a common target area. The software provides processor-executable instructions for determining acceptable timing and location for release of the plurality of mission stores, such as within the common target area, and such that the mission stores achieve communication with the respective mission reference points. The processor-executable instructions calculate and identify a common release area within the common target area, such as a composite launch acceptability region of overlap of separate target regions of each mission store, in addition to identifying an entrance and exit point of the composite region.

A method for securing a geographical area encompassing a route. A map of the area is obtained. A weapon is associated with a firing modeling consisting of a probability model of hitting its target when shooting, as a function of the firing distance. Positions of potential shelters of threats on the map are determined by using a trained artificial intelligence device. The modeling is applied for each weapon and potential shelter while relating the shots to the route and summing all the probabilities of hitting its target on each portion of the route. The potential shelters most likely to constitute attack threats along the route are determined. A path is defined in order to address these potential shelters most likely to constitute attack threats.

A flying vehicle is disclosed with a plurality of projectile systems that each contains a projectile for projecting at another flying device. The flying vehicle can include a control system, a flight system in communication with the control system for enabling the flying vehicle to fly, a first projectile system in communication with the control system and a second projectile system in communication with the control system. The control system determines, based on a characteristic of a target flying vehicle, whether to implement a first mode utilizing the first projectile system or a second mode utilizing the second projectile system to capture the target flying vehicle.

A feasibility display indicative of a feasibility of a weapon successfully engaging a target and/or a feasibility of a weapon successfully engaging the aircraft is generated. The aircraft in conjunction with another device cooperatively generate the same. The another device has a database describing a performance envelope of the weapon. The another device identifies a best candidate polynomial from a plurality based on scores of the plurality. Each score is based on a quality of fit of the candidate polynomial to a characteristic of the performance envelope of the weapon. The another device uploads, after a plurality of characteristics are evaluated, to the aircraft coefficients which are determined for the best candidate polynomial Variables of the plurality are some or all of a weapon or aircraft firing condition parameters The aircraft uses selected coefficients to generate the feasibility display where selection is based on conditions of the aircraft and target.

A system comprising an unmanned aerial vehicle (UAV) configured to transition from a terminal homing mode to a target search mode, responsive to an uplink signal and/or an autonomous determination of scene change.

Systems and methods include an unmanned aerial vehicle (UAV) having a body and a plurality of propulsion systems, a gimbal system having a plurality of targeting sensors and a warhead mount configured to carry and deploy a warhead, and a logic device. The logic device is configured to detect a target along a UAV flight path, track the target using sensed data from the targeting sensors, calculate an attack vector for the UAV to intercept the target, calculate a detonation angle for the warhead with respect to the attack vector and a selected location on the target, and instruct the gimbal system to orient the warhead at the detonation angle.

Systems, devices, and methods for identifying a target aerial vehicle, deploying an interceptor aerial vehicle comprising at least one effector, maneuvering the interceptor aerial vehicle to a position to engage a target aerial vehicle, deploying the at least one effector to intercept the target aerial vehicle, and confirming that the target aerial vehicle has been intercepted.