Launch and land system for a tethered aircraft (in connection with FIG. 1) The invention provides for a launch and land system (1) for a tethered aircraft (90) comprising a runway (12) for the aircraft and a winch (62) for the tether (92), wherein the runway comprises a funnel-shaped target area (14) with a wide end oriented towards one end of the runway and a narrow end opposite of the wide end, wherein said target area is laterally bordered by restriction devices (80) extending from one end of the target area to the other for preventing the aircraft to roll out of the target area.

The present invention relates to a fire fighting system for transporting a nozzle of a fire hose coupled to a drone to a high place. The fire fighting system includes a fire hose (10) having a fire hose (10) having a nozzle (11) for injecting a fire extinguishing liquid; a fire-extinguishing-liquid supply source (2) which is coupled to the fire hose (10), and supplies the fire extinguishing liquid to the fire hose (10); a top drone (1) coupled to the nozzle (11); a wired cable (4) coupled to the top drone (1); and a power supply unit (3) which supplies power or fuel for flying the top drone (1) through the wired cable (4).

A flying object with a landing gear module serving as a floating weight that can be used simultaneously with an airship and an aerial mooring type aerostat, and more particularly, a flying object capable of simultaneously allowing a landing gear to serve as a floating weight, thereby stably simplifying a mooring process of the flying object and manufacturing the flying object at low cost.

A flying object with a landing gear module serving as a floating weight that can be used simultaneously with an airship and an aerial mooring type aerostat, and more particularly, a flying object capable of simultaneously allowing a landing gear to serve as a floating weight, thereby stably simplifying a mooring process of the flying object and manufacturing the flying object at low cost.

Systems and methods are disclosed for package delivery using unmanned aerial vehicles. Example methods may include positioning a first component at a first elevation, and operatively connecting the first component to a winch; positioning a second component at a second elevation higher than the first elevation; and configuring cable of a lifting component to: operatively connect to the first component and the second component, connect to and disconnect from a vehicle, and lift the vehicle from the first component towards the second component using the winch.

A vehicle that may include an upper surface, a housing configured to store a drone, the housing having an opening that is formed outside the upper surface; a base that is configured to provide a landing spot to the drone when the base is positioned at least in part outside the housing, and to support the drone when the drone is positioned within the housing; and a base movement unit for moving the base through the opening and between an inside position and an outside position, wherein when the base is positioned in the inside position an area of the base allocated for supporting the drone is located within the housing, wherein when the base is positioned in the outside position the area of the base allocated for supporting the drone is located outside the housing.

The invention mainly relates to a device for automatically releasing, maintaining in flight, and recovering a tethered aerostat. The device includes a platform having a rotatably mobile part, a device for recovering the tethered balloon secured to the mobile part, and at least first and second winches. A first cable called umbilical cable is connected to the first winch and has an end provided to be secured to the aerostat. A second cable called sling is divided into at least an adapted mooring portion having an end provided to be secured to aerostat, and a connecting portion connected to the second winch, which connecting portion has a linear mass smaller than or equal to seven grams per meter and a length greater than that of the mooring portion.

A hybrid aircraft system uses a combination of direct propeller driven gas engine and electric motor power to provide vertical thrust and control for hover of the aircraft. Furthermore, a portable launch/recovery system is configured for use with an aircraft such as a Vertical Takeoff and Landing (VTOL) Unmanned Air Vehicle (UAV). The system is configured to enable ships with limited available deck space to become UAV-compatible.

Apparatus and methods are provided for providing persistent aerial vehicle surveillance capabilities, including launch and recovery platforms, secured communication, sensor systems, targeting systems, locating systems, and precision landing and stabilization systems for such uses as assisting with base defenses, monitoring parking lots or facilities, providing security monitoring, assisting farmers, performing recon of enemy beaches or use by mortar teams in hostile fields of operations. One embodiment can include an aerial surveillance system using an aerial short wave infrared surveillance system platform for use when quick response in reaction to real-time conditions is preferred while relaying the geo-location and other monitoring assistance via a wireless, fiber optic type link, or an ADHOC GPS system. Embodiments of this disclosure provides a user with precise targeting, without manned air assets, and a highly mobile base of operations with swift relocation possibilities in a denied or hostile environment.

A control device for controlling a kite steering arrangement, including a base, a control bar support extending downward on the base, a control bar pivot point mounted displaceably about the control bar support, a pair of interconnecting members extending between opposing end regions of the control bar and the base upper the control bar support, a tensioning mechanism, a base pivot point, a base rotator for allowing rotation of the base about a vertical axis thereof, a manipulator that manipulates the base pivot point and base rotator, and a communicator, that communicates adjustment of the interconnecting members to the kite steering arrangement. The length aspect of the interconnecting members is adjusted by pivoting the control bar about the control bar pivot point and/or by displacement of the control bar pivot point relative the control bar support.