The present invention pertains to a system and method for transportation of goods, service, marketable securities or other valuable payloads optionally utilizing a carrier or smart carrier to contain a payload and using artillery for transporting the payload relatively longer distances, whereby more conventional transportation systems may bring a payload to the artillery mechanism and then retrieve the payload from the artillery mechanism. The system consists of a modified military artillery projectile, optionally containing a self-monitoring smart carrier or a standard carrier, transportation shells for various transportation methods and when smart carriers are employed, goods and services and in some embodiments, people, on land, air and water through a connected ecosystem, may be monitored and safely transported. Modified military artillery is used to propel goods to discrete distance remote stations, alongside, in some examples, torpedoes, sniper rifles, and other long rage apparatuses, such as drones, mortars, and howitzers. The selection of what artillery to use is a function of availability and desired distance and performance, and the interaction with non-ballistic delivery systems, to and from the artillery or ballistic legs of the desired delivery pathway, are ones of optimal design and performance choice of a user of the present invention.

A vehicle comprising a morphing wing and a body is disclosed. The aircraft is configured to transform from a first configuration into a second configuration for ascent or descent of the aircraft. The drag force and lift force on the aircraft in the second configuration are less than in the first configuration. Transforming from the first to the second configuration comprises: contracting the wing within a geometric plane defined by the wing, and rotating the outer edge of the wing downwards, out of the geometric plane.

Autonomous behaviors in a multiagent adversarial scene, including: assigning, by a scene manager, to each friendly agent of plurality of friendly agents, a role comprising an engagement to an adversarial agent of one or more adversarial agents; assigning, by the scene manager, to each friendly agent of the plurality of friendly agents, a policy; and wherein each friendly agent of the plurality of friendly agents is configured to determine, based on a tactical model corresponding to the assigned policy, one or more actions.

An aircraft includes an airframe with first and second wings having a fuselage extending therebetween. A propulsion assembly is coupled to the fuselage and includes a counter-rotating coaxial rotor system that is tiltable relative to the fuselage to generate a thrust vector. First and second yaw vanes extend aftwardly from the fuselage. A flight control system is configured to direct the thrust vector of the coaxial rotor system and control movements of the yaw vanes. In a VTOL orientation of the aircraft, differential operation of the yaw vanes and/or differential operations of first and second rotor assemblies of the coaxial rotor system provide yaw authority for the aircraft. In a biplane orientation of the aircraft, collective operation of the yaw vanes provides yaw authority for the aircraft.

An aircraft includes an airframe with first and second wings having a fuselage extending therebetween. A propulsion assembly is coupled to the fuselage and includes a counter-rotating coaxial rotor system that is tiltable relative to the fuselage to generate a thrust vector. Tail assemblies are coupled to wingtips of the first and second wings each having an elevon that collectively form a distributed array of elevons. A flight control system is configured to direct the thrust vector of the coaxial rotor system and to control movements of the elevons such that the elevons collectively provide pitch authority and differentially provide roll authority for the aircraft in the biplane orientation. In addition, when the flight control system detects an elevon fault, the flight control system is configured to perform corrective action responsive thereto at a distributed elevon level or at a coordinated distributed elevon and propulsion assembly level.

A system for suppressing fires from an aircraft has a munition deployment system suspended beneath the aircraft. A shield is suspended between the aircraft and the munition deployment system to protect the aircraft. The munition deployment system has munitions compartments containing munitions for deploying vertically from the munition deployment system, and for detonating over a fire. A controller within the aircraft communications with a sensor package in the munition deployment system and directs the order of munition deployment.

An Unmanned Aerial Vehicle is disclosed. The Unmanned Aerial Vehicle includes a body, rotors attached to the body, one or more sensors, and an electromagnetic pulse transmitter. The electromagnetic pulse transmitter is configured to transmit an EMP and the Unmanned Aerial Vehicle is configured to track a target Unmanned Aerial Vehicle using the one or more sensors and direct the electromagnetic pulse transmitter at the target Unmanned Aerial Vehicle to disrupt the target Unmanned Aerial Vehicle.

A fragmentation warhead is provided, capable of being mounted in a carrier vehicle, the warhead having a longitudinal axis. In at least one example the warhead includes a shell that extends along the longitudinal axis. The shell includes a fixed shell portion and a fragmentation portion, and defines therebetween a cavity for accommodating therein an explosive charge. The fragmentation portion includes at least one set of serially adjacent fragments in correspondingly serially contiguous relationship in the fragmentation portion and in generally helical relationship with respect to the longitudinal axis. A corresponding carrier vehicle and a corresponding missile are also provided.

Systems and methods for countering an unmanned air vehicle are disclosed. An example method includes detecting a target UAV via a first component of a target acquisition system. The example method further includes, in response to detecting the target UAV, directing, by executing one or more computer-readable instructions of a launch control system in communication with the target acquisition system, an interceptor UAV to launch. The example method further includes, subsequent to the launch, tracking the target UAV via a second component of the target acquisition system, the second component carried by the interceptor UAV. The example method further includes, when the target UAV is within a target range of the interceptor UAV, deploying a disabling element from the interceptor UAV toward the target UAV.

Systems, apparatuses, and methods are provided herein for facilitating task assignments and communications. A task defining interface is provided on a user device associated with a task team member. Tasks are defined with a task request comprising a task identifier associated with a target location, a task instruction identifier comprising a first symbol followed by a task instruction, and a plurality of task team member identifiers each comprising a second symbol followed by a user handle, wherein the task instruction specifies one or more characteristics of the first task to be performed at the target location. The system is further configured to display tasks associated with a user account based on task team member identifiers and automatically communicate, via the task view interface, each of the one or more task instruction identifiers associated with the task record to each task team member associated with the task record.