Amphibious vertical takeoff and landing unmanned device

An amphibious vertical takeoff and landing (VTOL) unmanned device with an artificial intelligence (AI) data processing mobile and wearable apparatus, the amphibious VTOL unmanned device comprising:

• a modular and expandable waterproof body adapted for carrying a payload;
• an outer body shell associated with the modular and expandable waterproof body and comprising one or more pieces;
• a gimbaled swivel propulsion (GSP) system, the GSP system comprising a plurality of VTOL jet engines and VTOL ducted fans associated with a plurality of motors, wherein the plurality of VTOL jet engines are selected from turbojet engines, turbofan engines, and foldable variable pitch tilting engines, wherein the VTOL ducted fans include at least a multi-blade ducted fan, the plurality of VTOL jet engines being adapted for driving the amphibious VTOL unmanned device on a surface and in a flight, wherein the turbojet engines comprise afterburners configured to rotate a fuel jet with hydraulic actuator rotation and communicating with an engine fuel system of the amphibious VTOL unmanned device, the engine fuel system having a line management electro-hydraulic control converter mounted on the turbojet engines, wherein the afterburners allow for bursts of acceleration of the fuel jet;
• a processor, electronic speed controllers, a two-way telemetry device, a video transmitter, a radio control receiver, and a power distribution board, the processor being configured for controlling at least vectoring of a GSP thrust associated with the GSP system to control a direction of a thrust generated by the plurality of VTOL jet engines, wherein the electronic speed controllers are selected from a standalone electronic speed controller and an electronic speed controller integrated into the power distribution board;
• an electrical machine comprising a stator electrically connected to an electrical power storage device, wherein the electrical machine acts as an electric motor for driving rotation of the plurality of VTOL jet engines by using the electrical power storage device, and wherein the electrical machine with the plurality of VTOL jet engines act as an electrical power generator for re-charging the electrical power storage device;
• an onboard electricity generator comprising a plurality of solar cells, wherein the onboard electricity generator includes carbon fiber hybrid solar cells;
• printed parts selected from 3D printed parts and 4D printed parts;
• a light detection and ranging (LIDAR) device, an ultrasonic radar sensor, and a plurality of sensors;
• a tail attached to the modular and expandable waterproof body at a rear end and adapted for stabilizing the amphibious VTOL unmanned device;
• a head VTOL ducted fan attached to the modular and expandable waterproof body at a front end and adapted for VTOL;
• a plurality of wheels at a bottom of the amphibious VTOL unmanned device connected to the power distribution board;
• a plurality of foldable wings on sides of the modular and expandable waterproof body, the plurality of foldable wings being adapted for creating a pressure difference and creating a lift associated with the amphibious VTOL unmanned device;
• and
• a plurality of parachutes attached to the amphibious VTOL unmanned device to safely land the amphibious VTOL unmanned device in an emergency, wherein at least one parachute of the plurality of parachutes is fixed to each of:
• the bottom of the amphibious VTOL unmanned device, the front end of the amphibious VTOL unmanned device, and the rear end of the amphibious VTOL unmanned device.