A collision avoidance system for an airplane under tow may include a sensing device configured to capture image data of at least a portion of the airplane and an object while the airplane is being towed. The sensing device may be located remotely to both the airplane and the object. Positions of two or more features of the airplane may be determined based on the image data. A bounding box encompassing the airplane may be generated based, at least in part, on the positions of the two or more features. Additionally, based on a comparison of the position of an object relative to the bounding box, it may be determined whether the object is within a predetermined distance from the airplane.

A system and method for participating in a multi-USV performance in three-dimensional space. The USV can include: a location identification system operable to provide location coordinates, a guidance system operable to guide the USV toward target waypoints, a propulsion system operable to propel the USV, a power supply operable to provide power to components of the USV, and an exoskeleton surrounding the location identification system, the guidance system, the propulsion system, and the power supply, the exoskeleton including a set of sensory devices, and at least one latching mechanism operable to facilitate a docking operation with a proximate USV.

An obstacle advisory system for a vehicle and a method for operating the same are provided. The system, for example, may include, but is not limited to a display, and a processor communicatively coupled to the display, the processor configured to receive sensor data from at least one sensor configured to sense obstacles around a vehicle, generate obstacle display data based upon the sensor data, the obstacle display data comprising display data for each of a plurality of sectors and for each of a plurality of blocks within each of the plurality of sectors forming a grid surrounding the vehicle, and display the generated obstacle display data on the display.

An amphibious vertical takeoff and landing (VTOL) unmanned device is provided. The amphibious VTOL unmanned device includes a modular and expandable waterproof body, an outer body shell, a gimbaled swivel propulsion system comprising a plurality of VTOL jet engines and VTOL ducted fans, a processor, electronic speed controllers, a two-way telemetry device, a video transmitter, a radio control receiver, a power distribution board, an electrical machine, an onboard electricity generator comprising a plurality of solar cells, a light detection and ranging device, an ultrasonic radar sensor, a plurality of sensors, a tail configured to stabilize the amphibious VTOL unmanned device, a head VTOL ducted fan adapted for VTOL, a plurality of wheels, a plurality of foldable wings configured to create a pressure difference and creating a lift, a plurality of parachutes configured to safely land the amphibious VTOL unmanned device in an emergency.

A method to provide negotiation control to data such that a person or entity can negotiate the use of data gathered beyond what is needed for a particular use by a third party transaction. The method also provides negotiation for the control and operation of autonomous vehicles such as drones operating in non-public space.

Embodiments of the present invention provide an aircraft for vertical take-off and landing. In various embodiments, an aircraft assembly includes at least one first wing portion providing a lift force during a horizontal flight, at least one wing opening disposed on a vertical axis of the at least one first wing portion and at least one thruster positioned inside the at least one wing opening to provide vertical thrust during a vertical flight. The aircraft assembly can further include air vents positioned inside at least one of the wing openings. The air vents can further include louvres positioned over or under the air vents to open and close the wing openings. The thruster can further be used to provide flight control for the aircraft.

An anti-collision system for an UAV and a method thereof are provided. The anti-collision system for an UAV includes: a first aerial vehicle. The first aerial vehicle includes: a wireless transmission module and a processor. The wireless transmission module is used for transmitting a first signal of the first aerial vehicle and for receiving a second signal from a second aerial vehicle; the processor is used for calculating a signal strength of the second signal, for obtaining a spacing distance between the second aerial vehicle and the first aerial vehicle, to determine if the spacing distance is less than a distance threshold value; wherein when the spacing distance is less than the distance threshold value, the processor adjusts a flight status of the first aerial vehicle. Thus the present invention can avoid the collisions between the first aerial vehicle and the second aerial vehicle.

Presented are a method, apparatus, and computer-readable medium for gathering information. An exemplary apparatus includes at least one processor and a memory storing computer instructions executable by the at least one processor, wherein the memory with the computer instructions and the at least one processor are configured to cause the apparatus to at least receive a flight path from a predetermined location to a location of an emergency. The apparatus is further caused to travel the flight path from the predetermined location to the location of the emergency, capture information at the location of the emergency, and transmit the captured information.

A system and method for management of airspace for unmanned aircraft is disclosed. The system and method comprises administration of the airspace including designation of flyways and zones with reference to features in the region. The system and method comprises administration of aircraft including registration of aircraft and mission. A monitoring system tracks conditions and aircraft traffic in the airspace. Aircraft may be configured to transact with the management system including to obtain rights/priority by license and to operate in the airspace under direction of the system. The system and aircraft may be configured for dynamic transactions (e.g. licensing/routing). The system will set rates for licenses and use/access to the airspace and aircraft will be billed/pay for use/access of the airspace at rates using data from data sources.

Example aircraft intent processors are described herein that can be used both for the prediction of an aircraft's trajectory from aircraft intent, and the execution of aircraft intent for controlling the aircraft. An example aircraft intent processor includes an aircraft intent input to receive aircraft intent data representative of aircraft intent instructions, an aircraft state input to receive state data representative of a state of the aircraft, and a residual output. The aircraft intent processor is to calculate residual data representative of an error between a state of the aircraft commanded by the received aircraft intent data and the state of the aircraft expressed by received state data, and output the residual data via the residual output.