Disclosed herein is a vehicular system, in accordance with some embodiments. Accordingly, the vehicular system may include a body, a rotatable head, a plurality of devices, a propulsion assembly, at least one actuator, a power source, and a controller. Further, the rotatable head rotatably coupled to the body. Further, the plurality of devices mounted on the rotatable head. Further, the plurality of devices may include a grabber device and at least one sensing device. Further, the propulsion assembly coupled to the body. Further, the propulsion assembly may be electrically powered. Further, the at least one actuator operationally coupled to the rotatable head. Further, the at least one actuator may be configured to perform at least one actuator operation. Further, the power source electrically coupled to the at least one actuator and a propulsion assembly. Further, the controller communicatively coupled to the at least one actuator.

Disclosed herein is a vehicular system, in accordance with some embodiments. Accordingly, the vehicular system may include a body, a rotatable head, a plurality of devices, a propulsion assembly, at least one actuator, a power source, and a controller. Further, the rotatable head rotatably coupled to the body. Further, the plurality of devices mounted on the rotatable head. Further, the plurality of devices may include a grabber device and at least one sensing device. Further, the propulsion assembly coupled to the body. Further, the propulsion assembly may be electrically powered. Further, the at least one actuator operationally coupled to the rotatable head. Further, the at least one actuator may be configured to perform at least one actuator operation. Further, the power source electrically coupled to the at least one actuator and a propulsion assembly. Further, the controller communicatively coupled to the at least one actuator.

Autonomous underwater vehicles and systems are provided with fast stabilization and fine attitude control with a constant and high rotational speed flying wheel to rotate the vehicle's body with respect to its core and optionally a combination of reaction masses used in three perpendicular axes. The gimbal and the reaction mass inertial systems are used for fast response to any angular or linear disturbance coming from the ocean current or waves. When equipped for optical communications, the vehicle has an optical receiver and transmitter and controller that provides three levels of attitude stabilization: gimbal and the reaction mass inertial systems; isolated movable platform and fine optical beam steering for targeting the laser beam from the transmitter. The ability to maintain precise positioning allows multiple vehicles to be optically linked.

Autonomous underwater vehicles and systems are provided with fast stabilization and fine attitude control with a constant and high rotational speed flying wheel to rotate the vehicle's body with respect to its core and optionally a combination of reaction masses used in three perpendicular axes. The gimbal and the reaction mass inertial systems are used for fast response to any angular or linear disturbance coming from the ocean current or waves. When equipped for optical communications, the vehicle has an optical receiver and transmitter and controller that provides three levels of attitude stabilization: gimbal and the reaction mass inertial systems; isolated movable platform and fine optical beam steering for targeting the laser beam from the transmitter. The ability to maintain precise positioning allows multiple vehicles to be optically linked.

An underwater drone is disclosed. The underwater drone includes a horizontal propeller module and a vertical propeller module to respectively provide a drone body with a horizontal proceeding force and a vertical lifting or diving force. The underwater drone includes a horizontal channel and a vertical channel, which allow the water to pass through for reducing resistance when the underwater drone moves forwards, upwards or downwards. The underwater drone is equipped with a buoy member with an antenna portion of a communication module disposed therein. The underwater drone is equipped with the fishing device, the fish finding device and the image capturing module. Therefore, the underwater drone is capable of fishing, rapidly moving and wireless remote control.

An underwater drone is disclosed. The underwater drone includes a horizontal propeller module and a vertical propeller module to respectively provide a drone body with a horizontal proceeding force and a vertical lifting or diving force. The underwater drone includes a horizontal channel and a vertical channel, which allow the water to pass through for reducing resistance when the underwater drone moves forwards, upwards or downwards. The underwater drone is equipped with a buoy member with an antenna portion of a communication module disposed therein. The underwater drone is equipped with the fishing device, the fish finding device and the image capturing module. Therefore, the underwater drone is capable of fishing, rapidly moving and wireless remote control.

A fixed-wing aerial underwater vehicle includes a shell component, a flight component and a pneumatic buoyancy component. The flight component includes a fixed wing and rotors, and the fixed wing and the rotors are mounted in the shell component. The pneumatic buoyancy component includes an air bladder and an inflation and deflation portion, and the inflation and deflation portion can inflate and deflate the air bladder. The air bladder is installed on the shell component, a containing space is formed in the shell component, and the inflation and deflation portion is partially or entirely installed in the containing space. Each rotor includes a rotor supporting rod, a motor base, a motor and a propeller, which are sequentially connected. A control method for the fixed-wing aerial underwater vehicle mentioned above is further provided.

A fixed-wing aerial underwater vehicle includes a shell component, a flight component and a pneumatic buoyancy component. The flight component includes a fixed wing and rotors, and the fixed wing and the rotors are mounted in the shell component. The pneumatic buoyancy component includes an air bladder and an inflation and deflation portion, and the inflation and deflation portion can inflate and deflate the air bladder. The air bladder is installed on the shell component, a containing space is formed in the shell component, and the inflation and deflation portion is partially or entirely installed in the containing space. Each rotor includes a rotor supporting rod, a motor base, a motor and a propeller, which are sequentially connected. A control method for the fixed-wing aerial underwater vehicle mentioned above is further provided.

Disclosed is a self-balancing control method for an unmanned underwater vehicle (UUV) that includes: fitting the UUV vehicle with at least one reversible propeller; converting the forces the unmanned underwater vehicle is subjected to into a resultant force in each of at least one degree of freedom (DOF) of motion based on a DOF of motion control model, where each of the DOF of motion corresponds to a measurable motion control parameter; designing a corresponding sub-PID controller according to each of the at least one DOF of motion; and calculating the thrust required by each of the at least one reversible propeller based on a thrust distribution matrix.

Disclosed is a self-balancing control method for an unmanned underwater vehicle (UUV) that includes: fitting the UUV vehicle with at least one reversible propeller; converting the forces the unmanned underwater vehicle is subjected to into a resultant force in each of at least one degree of freedom (DOF) of motion based on a DOF of motion control model, where each of the DOF of motion corresponds to a measurable motion control parameter; designing a corresponding sub-PID controller according to each of the at least one DOF of motion; and calculating the thrust required by each of the at least one reversible propeller based on a thrust distribution matrix.