Methods and apparatus for pointing logic in aircraft are disclosed. A disclosed example apparatus to aim an aiming device carried by an aircraft includes at least one memory, machine readable instructions, and processor circuitry. The processor is to at least one of instantiate or execute the machine readable instructions to determine a position of a target, determine an orientation of the aircraft, determine aiming points based on the orientation and a movement range of the aiming device, and determine a movement of at least one of the aircraft or the aiming device based on the aiming points and the position to orient the aiming device toward the target.

Disclosed herein is a payload delivery device. The payload delivery device is configured for delivering an explosive component. The payload delivery device comprises a first module having an interior cavity for containing an explosive component. The payload delivery device further comprises at least one attachment module connected to the central module via a connection means. The at least one attachment module having an interior cavity for containing an additional component.

A method for destroying enemy targets is disclosed which comprises the following steps: (a) carrying a multicopter drone in a backpack of a first soldier; (b) removing the multicopter drone from the backpack, unfolding, and coupling a weapon to the multicopter drone capable of carrying more than 12 kg; (c) remote controlling the multicopter drone to search for the enemy targets using a remote control; and (d) launching the missile from the multicopter drone when the enemy targets are detected.

A radio controlled (RC) vehicle includes a receiver that is coupled to receive an RF signal from a remote control device, the RF signal containing command data in accordance with a first coordinate system, wherein the first coordinate system is from a perspective of the remote control device. A motion sensing module generates motion data based on the motion of the RC vehicle. A processing module transforms the command data into control data in accordance with a second coordinate system, wherein the second coordinate system is from a perspective of the RC vehicle. A plurality of control devices control the motion of the RC vehicle based on the control data.

A radio controlled (RC) vehicle includes a receiver that is coupled to receive an RF signal from a remote control device, the RF signal containing command data in accordance with a first coordinate system, wherein the first coordinate system is from a perspective of the remote control device. A motion sensing module generates motion data based on the motion of the RC vehicle. A processing module transforms the command data into control data in accordance with a second coordinate system, wherein the second coordinate system is from a perspective of the RC vehicle. A plurality of control devices control the motion of the RC vehicle based on the control data.

Embodiments of a payload attachment system secure a missile, a suicide drone, or other ordinance to a wing or fuselage of a combat drone (or another type of aircraft) using one or more vacuum mounting modules, wherein each vacuum mounting module comprises at least one vacuum pump controllably coupled to a microcontroller, a vacuum cup fluidly coupled to the at least one vacuum pump, and a transceiver that receives an instruction corresponding to one of a vacuum cup actuation signal or a vacuum cup release signal.

A Munitions Payload Delivery System (MPDS) is provided. One embodiment of the MPDS comprises a multi-rotor drone configured to carry a munition in the form of a HEDP linear-shaped charge or Armor Piercing munition or other-shaped munition. The drone, in one embodiment, includes a camera that provides a remote operator with a real-time video feed so the operator can pilot the drone to a specific target on a battlefield. Once a target is selected, the operator ignites the munition by flying the drone into the target, landing the drone on the target, or activating a radio fire button. In one embodiment, each of these mechanisms closes a switch on board the drone connecting a voltage to a blasting cap inside the payload.

Systems and methods for targeted operational disablement that may utilize, for example, UAV-delivered shaped charges coupled to specific features of a target object. A UAV may navigate to, identify, and attach a disabling device to a critical component of a target such as a barrel of a tank main gun, a crew hatch cover, a tank tread, an engine compartment, or a magazine.

A Munitions Payload Delivery System (MPDS) is provided. One embodiment of the MPDS comprises a multi-rotor drone configured to carry a munition in the form of a HEDP linear-shaped charge or Armor Piercing munition or other-shaped munition. The drone, in one embodiment, includes a camera that provides a remote operator with a real-time video feed so the operator can pilot the drone to a specific target on a battlefield. Once a target is selected, the operator ignites the munition by flying the drone into the target, landing the drone on the target, or activating a radio fire button. In one embodiment, each of these mechanisms closes a switch on board the drone connecting a voltage to a blasting cap inside the payload.

A modular system for drones is provided. A chassis can include a coupling mechanism operable to removably couple the chassis with a drone. A plurality of modular components can be operable to be interchangeably coupled with a control component. The modular components can be operable to be detachably coupled with a payload.