Abstract: Disclosed is an unmanned, autonomous, cargo transport system comprising at least one towed aircraft coupled to a tractor aircraft for inflight towing.

Abstract: A fixed-wing cargo aircraft having a kinked fuselage to extend the useable length of a continuous interior cargo bay while still meeting a tailstrike requirement is disclosed. The fuselage defines a continuous interior cargo bay along a majority of its length and a pitch axis about which the cargo aircraft rotates during takeoff while still on the ground. The fuselage includes a forward portion defining longitudinal-lateral plane of the cargo aircraft an aft portion extending aft from the pitch axis to the aft end and containing an aft region of the continuous interior cargo bay that extends along a majority of a length of the aft portion. The aft portion has a centerline extending above the forward upper surface of the aircraft.

Abstract: The present disclosure provides an end-to-end cargo handling system. The end-to-end cargo handling system comprises a transportation unit comprising a first sensing agent, a lift unit comprising a second sensing agent, and a control module in communication with the transportation unit and the lift unit via a network, wherein the transportation unit and the lift unit are configured to move a cargo unit from a first location to a second location autonomously.

Abstract: The present invention provides a unique system to deliver packages from aerial vehicles to the ground through the use of a sophisticated guidance system and impact-absorbing catching mechanism. The new systems and methods of the present invention provide package delivery from manned and unmanned aircraft that is fully automated and reliably accurate to deliver a package to a ground station operable to receive the package in the catching mechanism.

Abstract: A high-place observation device for stably performing a fixed-point observation of a target object from a high place is provided. The high-place observation device provides [Solution] Provides a long pole which is formed to extend and contract freely and which stands on the installation surface, a rotorcraft for positioning the pole to a desirable height position by extending and contracting the pole by a floating force in a connected state, a winding mechanism which fixes and maintains the height position of the pole to the height position set by the rotorcraft, and a camera attached to the rotorcraft.

Abstract: An imaging system has a tether sub-system deployable and retrievable from an aircraft, an imaging device attached at a deployable end of the tether, and control apparatus comprising control and communication circuitry receiving images captured by the imaging apparatus and storing the images. The tether is deployed to a predetermined length, the aircraft is piloted in a flight pattern causing the imaging device at the deployed end of the tether to attain a fixed position proximate an imaging target, and the control apparatus is operated to capture images of the target.

Abstract: A cargo restraint assembly may comprise a first bracket slidingly coupled to a housing. A retention block may be pivotably coupled to the first bracket. A second bracket may be slidingly coupled to the housing. The first bracket may be coupled to the second bracket via a spring. The first bracket and the second bracket may be configured to attenuate in response to a cargo deck bending during transportation of cargo in an aircraft.

Abstract: A cargo handling system is disclosed. In various embodiments, the cargo handling system includes a first rail defining an upward facing surface and a longitudinal direction and a lateral direction; a platform having a first recessed channel configured to engage an upper portion of the first rail to prevent a movement of the platform in the lateral direction and configured for rolling engagement with the first rail; and a first drive assembly disposed within the platform and configured to propel the platform along the first rail in the longitudinal direction, the first drive assembly having a first drive roller and a first motor.

Abstract: A system for delivering objects from a fixed-wing aircraft has a first tether having a connector on a deployed end, an anchor apparatus fixed to a point on the ground, a slide ring assembled over the first tether, a drag line connected to the slide ring by one end, and a drag-producing device connected to at a second end, and an object carrying apparatus connected by a support line. The aircraft is flown at an altitude in an orbit at a diameter and a speed such that the deployed first tether assumes a spiral pattern. An object is placed in the object-carrying apparatus and released from the aircraft, with the slide ring guiding along the first tether, and the drag-producing element slows descent of the object in the carrying apparatus in the spiral pattern until the object reaches the ground, where the object is removed from the object-carrying apparatus.

Abstract: A sorting system has a sorting area and a controller system that receives luggage-related sorting information for each piece of luggage. A transport mechanism transports the luggage into a sorting area which includes a sorting area with at least one make-up-place connected to the transport mechanism. The make-up-place sorts the luggage according to at least one item of luggage-related sorting information. Movable load devices receive the pieces of luggage sorted by the at least one make-up-place. The controller system assigns each piece of luggage according to at least one luggage-related information to a particular movable load device and the controller system is also adapted to select a make-up-place for each piece of luggage and to send the piece of luggage to the selected make-up-place to be loaded into the assigned movable load device.

Abstract: A stiffener skeleton that is configured to be mounted to an upper deck of a rotary wing aircraft in a maintenance phase, comprising an upper stiffening structure with a plurality of supporting arms for providing upside stiffening support, and a lateral stiffening structure with a plurality of supporting legs for providing lateral stiffening support, wherein the plurality of supporting arms and the plurality of supporting legs form a self-supporting frame structure.

Abstract: A personnel rescue system has a winch subsystem comprising a first tether deployable and retrievable with a powered winch, a powered and controllable end effector attached at a deployable end of the first tether, a second tether attached by a first end to the end effector, a personnel harness attached at a second end of the second tether; and control apparatus in communication with the end effector, the control apparatus operable to maneuver the end effector vertically and laterally, carrying the personnel harness to a subject to be rescued.

Abstract: A data delivery system has a tether deployable from an aircraft having a first data repository, a transmission pod at a deployed end of the tether, the transmission pod having first wireless communication circuitry, a communication conductor in parallel with the tether connecting the data repository in the aircraft with the first wireless communication circuitry in the transmission pod, and a receiving station on ground surface having a receiving antenna, second wireless communication circuitry compatible with the first wireless communication circuitry in the transmission pod, and a second data repository. The tether is deployed from the aircraft in a manner to position the transmission pod stationary proximate the receiving station antenna, and data is downloaded from the data repository in the aircraft to the data repository in the receiving station via the communication conductor and the wireless communication circuitry in the transmission pod.

Abstract: An assembly includes at least one first collection of a plurality of spacecraft intended to be fastened to a launcher during a launch phase, wherein the spacecraft are arranged about a central axis (Z) in a given transverse plane perpendicular to the central axis, the spacecraft having edges along a longitudinal axis and being moreover arranged in such a way that a spacecraft is linked to a neighboring spacecraft of the collection by one edge by means of at least one fastener (B) positioned on the edge, so as to mechanically hold the spacecraft to one another, and a satellites-launcher adaptor to which the spacecraft are fastened in a transverse plane.

Abstract: A stabilizing system for a winch cable has a winch cable deployed and suspended from a helicopter, a cargo support attached at a deployed end of the winch cable, an end effector attached to the winch cable, the end effector comprising thrusters directed in a plurality of directions orthogonal to a vertical axis of the winch cable, first control circuitry in the helicopter, and second control circuitry in the end effector. Thrust of individual thrusters is controlled through the first and second control circuitry maintaining the axis of the winch cable vertical, damping swinging of the cable.

Abstract: A system for performing work on electrical power lines and/or splices on electrical power lines comprises an unmanned aerial vehicle (UAV), a power line tool adapted to perch on an electrical power line and/or a splice on an electrical power line, a support frame selectively releasably attached to the UAV, and a plurality of flexible dielectric support lines attaching the power line tool to the support frame. Each of the support lines are attached to a corresponding attachment point on the support frame and a corresponding attachment point on the power line tool.

Abstract: Cargo may be optimally placed within a cargo hold using a cargo mover comprising a flexible conveyor belt extending from a ground location to a cargo hold, data defining a dimensional map of available space existing within the cargo hold for placement of cargo, a conveyor controller operatively in communication with the flexible conveyer belt and comprising packing software, and a smart loader comprising a predetermined set of scanning sensors operative to scan the cargo hold and a processor operatively in communication with the predetermined set of sensors and the conveyor controller. An interior of the cargo hold is scanned to create a dimensional map of the cargo hold and cargo placed onto the flexible conveyor belt where certain of each piece is cargo's physical dimensions are scanned.

Abstract: Systems and methods for an unmanned aerial vehicle (UAV) and control are provided. A UAV may include a swashplateless and hinged propulsion system, and a rotating payload system including an ISR device, a wind sensor, explosive charge and an atmospherics and/or CBRN sensor. A UAV flight controller may include a motion, compass, visual and gyroscopic (MCVG) or other gravitational forces sensor, a communications module configured to communicate with a UAV, and a flight module. The flight module may be configured to receive flight data from the UAV and generate flight control instructions based at least on the flight data and data received from the MCVG sensor. The flight control instructions may be operable to pilot the UAV based on movement of the UAV flight controller in 3D space.

Abstract: A high-place observation device for stably performing a fixed-point observation of a target object from a high place is provided. The high-place observation device provides a long pole which is formed to extend and contract freely and which stands on the installation surface, a rotorcraft for positioning the pole to a desirable height position by extending and contracting the pole by a floating force in a connected state, a winding mechanism which fixes and maintains the height position of the pole to the height position set by the rotorcraft, and a camera attached to the rotorcraft.

Abstract: A cargo hold comprises at least one luggage holder having at least one luggage compartment, wherein, when the hatch is in the closed state, the luggage holder is arranged in the cargo hold, and wherein, when the hatch is in the opened state, the luggage holder can be brought out of the cargo hold and can be introduced therein again by means of a guide mechanism in such a manner that the luggage holder, when it is brought out of the cargo hold, is arranged substantially radially to the substantially elliptical cross section of the fuselage.

Abstract: A loading frame includes a base and two walls arranged on opposite sides of the base. The walls are flexible and are arranged to permit movement, preferably sliding, between the wall and the load space's side, the wall being supported on the side. A system and a method for loading articles utilize the loading frame.

Abstract: An aircraft passenger seating unit and aircraft seating arrangements including seating units, each seating unit configured as a window-facing seating unit or as an aisle-facing seating unit. Each individual seating unit including first and second laterally adjacent seats mounted on a common platform and oriented at an angle to a longitudinal aircraft axis. A forwardmost point of each of the first and second seats, when in an upright sitting position, resides along a plane common to both the first and second passenger seats perpendicular to the longitudinal aircraft axis to allow longitudinal alignment of rows and increased seating density.

Abstract: A boarding pass may include a barcode with an encoded seat identifier. An overhead storage system may include a barcode reader configured to read the barcode of the boarding pass. The system may determine whether the boarding pass is eligible to access an overhead bin based on the encoded seat identifier. Where the boarding pass is eligible, a signal may be sent to one or more actuators of the overhead bin. Thus, a user may selectively access the overhead bin by the boarding pass.

Abstract: Disclosed is an unmanned automated hook-fastening device including a device coupler, a propulsion unit, a transmitter, a receiver, hook pliers, and an unloading transmitter. The propulsion unit adjusts the position of the hoisting unit with respect to the object, on the basis of the position signal transmitted by the transmitter and received by the receiver, and adjusts the position of the hoisting unit coupled to the object, on the basis of the position signal transmitted by the unloading transmitter and received by the receiver. It is possible to easily track the position of a hook of the object to be hoisted, automatically fasten the hook pliers to the hook, and automatically fasten the hook to a crane without a monitoring system.

Abstract: A cargo loading platform for an aircraft, with a plate-like supporting structure, which is configured to support or to receive cargo, and a lifting device. The lifting device is arranged asymmetrically on the plate-like supporting structure and can be moved from a stowage position to a lifting position. In the stowage position, the lifting device is arranged here above a lower side of the plate-like supporting structure and, in the lifting position, is at least partially arranged below the lower side of the plate-like supporting structure. This permits asymmetrical raising of the plate-like supporting structure by the lifting device, as a result of which steps during the transportation of the cargo loading platform can be easily and rapidly overcome. Furthermore, a cargo loading apparatus and a cargo container each with such a cargo loading platform, and also an aircraft with such a cargo loading apparatus are described.

Abstract: An aircraft comprises a weapons bay, the weapons bay comprising a cavity having an opening through which stores may be deployed, and a door assembly for exposing/closing the opening of the cavity. A first store is held in the cavity via a launcher and a first structure is disposed inside the cavity, for controlling the aero-acoustic environment. The first structure for controlling the aero-acoustic environment is removeably mounted in the weapons bay, such that if the first store is exchanged for a second, different, store, the structure for controlling the aero-acoustic environment may be unmounted from the weapons bay and removed, to be exchanged for a second, different, structure for controlling the aero-acoustic environment.

Abstract: Anti-collision airport system including a motorized mobile device to be moved close to an aircraft. The system includes a database to record structural characteristics of categories of aircraft and structural characteristics of the motorized mobile device. The controller is configured to identify a category corresponding to the aircraft and a positioning of the motorized mobile device with respect to the aircraft, search and retrieve, from the database, structural characteristics associated with the category corresponding to the aircraft and structural characteristics of the motorized device, calculate a trajectory for the movement of the motorized mobile device on the basis of the structural characteristics of the aircraft and of the motorized mobile device and of the positioning of the motorized mobile device with respect to the aircraft, and control the motorized mobile device according to the calculated trajectory.

Abstract: Embodiments of the present disclosure are directed to systems and methods for autonomously performing and/or facilitating drone diagnostic functions. Prior to a mission of a UAV, an inspection station comprising at least one imaging sensor and at least one directional force sensor may be used to perform a plurality of air worthiness inspections and/or maintenance checks with little to no human intervention. Once the UAV has been determined to be air worthy, it is approved for a subsequent mission.

Abstract: A device for refueling an aircraft, including a fuel flow duct, the downstream end of which is equipped with a wing coupler for connecting it to an inlet orifice of a fuel tank of the aircraft. The wing coupler includes a body, and a front valve that is movable with respect to the body. The wing coupler includes at least one detection member for detecting the position of the front valve, and an electrical or electronic transmission system for transmitting to a processing unit a signal representing the position of the front valve as detected by the at least one detection member.

Abstract: A modular aerial cargo aerodynamic encasement and a method for modular aviation cargo transport is provided. The aviation cargo aerodynamic encasement comprises a platform having a planar upper surface configured to accept cargo and a lower surface. The lower surface includes two or more ground supports displacing a portion of the platform from contact with a supporting surface. The platform includes two or more load transfer structures. The aviation cargo aerodynamic encasement further comprises a fairing configured to detachably couple to the platform, wherein the fairing, when coupled to the platform, forms an aerodynamic encasement, and wherein the aerodynamic encasement is detachably mountable to an aircraft by the two or more load transfer structures.

Abstract: An aircraft configured to drop an object includes a body, a cavity defined in the body and opening on a bottom face of the body, and a gas supply part configured to blow gas from vertically above to a blowing position on the object which is detachably mounted in the cavity. The blowing position is a position on a side closer to a nose of the aircraft with respect to a center of gravity of the object.

Abstract: A PDU for use in an aircraft includes a wheel configured to convey cargo through a portion of the aircraft. The PDU further includes an armature rotatably coupled to the wheel. The PDU further includes a brake pad. The PDU further includes a hold solenoid configured to compress the armature against the brake pad by a brake amount in order to apply a hold braking force to the wheel by resisting rotation of the armature. The PDU further includes a release solenoid configured to apply a force to separate the armature from the brake pad in order to allow the armature to rotate. The PDU further includes a magnet configured to compress the armature against the brake pad by a drag amount that is less than the brake amount in order to apply a drag braking force to the wheel by resisting rotation of the armature.

Abstract: A vehicle cabin seat arrangement includes a seat rail having a first and a second side faces; a group of passenger seats held on the seat rail by holding devices resting on a top side of the seat rail; pluralities of first and second holding blocks arranged on the first and second side faces, respectively; and a plurality of stop blocks arranged on a bottom side of a holding device To every passenger seat two first or second holding blocks are assigned, between which a holding device coupled with the passenger seat is displaceable. The respective holding device, includes one of the stop blocks arranged on the bottom side of the holding device such that the stop block is bringable into contact with the two assigned holding blocks on moving the holding device on the seat rail. Passenger seats are alternatingly assigned with first and second holding blocks.

Abstract: In some embodiments, systems, apparatuses and methods are provided herein that enable delivery of retail products. Some embodiments provide delivery systems comprising: a package support frame comprising first and second package supports, and a pivot coupler pivotably securing the first package support with the second package support; and a first release plate positioned across a separation between the first and second package supports, and comprising: a set of at least one angled locking grooves; a set of at least one groove pins slidably positioned within a respective one of the locking grooves; and a release tab configured to contact a surface and cause an unlocking of the first release plate such that the release plate moves with the locking grooves sliding along respective groove pins such that the base of the package support pivots away from the base of the second package support enlarging a package release aperture.

Abstract: A system to maintain a phase difference is disclosed. Two or more aircraft fly in a continuous periodic trajectory. The system maintains a phase difference between the two or more aircraft. Telemetry information for a reference aircraft moving in a first periodic trajectory is received. A phase difference between a primary aircraft and the reference aircraft with respect to the first periodic trajectory is determined. A variance in the phase difference between the primary aircraft and the reference aircraft from the target phase difference is determined. A new trajectory for the primary aircraft that decreases the variance in the phase difference with respect to the new periodic trajectory is determined, and the primary aircraft is maneuvered to follow the new trajectory.

Abstract: Embodiments includes a system and method for automatic orientation of a display for a portable electronic device (PED) of an aircraft cargo control and monitor panel. The system includes an attitude heading reference system for detecting a first heading information, a master control panel operably coupled to the attitude heading reference system, and a portable electronic device operably coupled to the master control panel. The PED includes a sensor for detecting a second heading information, a display, and a processor operably coupled to the sensor and the display. The processor is configured to receive the first heading information, receive the second heading information, where the first heading information is different than the second heading information, compare the first heading information and the second information, and modify an orientation of a presentation of the display based at least in part on the comparison.

Abstract: An adjustable cable attachment system for a VTOL aircraft includes a VTOL airframe. A winch is operatively connected to an underside of the airframe with the aircraft in a horizontal flight mode. An adjustable cable is operatively connected to the winch to adjustably relocate a slung load with respect to the center of gravity of the aircraft to balance the aircraft. A fixed cable is operatively connected to the underside of the airframe with the aircraft in the horizontal flight mode.

Abstract: A cover is configured to selectively engage with a portion of a structure in response to receiving a wireless electrical power signal at a receiver antenna of the cover from a wireless power source located in an outside environment, to separate a first environment on a first side of the cover from a second environment on a second side of the cover opposite the first side. In response to wirelessly receiving the electrical power signal, a fastening subassembly of the cover changes from a secured mode configured to inhibit opening a cover body with respect to the structure, to an unsecured mode configured to facilitate opening the cover body with respect to the structure. This in turn allows the cover to be matingly engaged with a portion of the structure to form a smooth continuous surface, without any exposed fasteners on the exterior side of the cover.

Abstract: A stackable cargo container apparatus has a frame assembly formed by interconnected structural members, a substantially planar base, interconnecting side walls and at least one personnel access door. At least one lifting harness member of unitary or singular construction is operationally attached to the frame assembly, and permits lifting of the cargo container apparatus from its bottom and away from welds or other possible weak points. An integrated cargo weight measurement assembly permits quick and efficient determination of cargo weight placed on the planar base, and includes a digital display or other output device.

Abstract: A mono-rail crane system (and a corresponding operation method) for use in an aircraft. The crane system comprises a first longitudinal mono-rail installable on the underside of a rear cargo door of the airplane parallel to the longitudinal axis of the rear cargo door; a second longitudinal mono-rail, which is installable on a cargo hold ceiling of the aircraft, and, in the fully opened state of the rear cargo door, in aligned continuity with the first longitudinal mono-rail so that the longitudinal axes of the first and second longitudinal mono-rails coincide to form one common longitudinal axis; a crane mobile equipment configured to be moved along the first and second longitudinal mono-rails in order to hoist and transfer the load; and a linear actuator configured to advance and retreat the second longitudinal monorail towards and away from the first longitudinal monorail.

Abstract: The present disclosure provides systems and methods for predicting the future locations of objects that are perceived by autonomous vehicles. An autonomous vehicle can include a prediction system that, for each object perceived by the autonomous vehicle, generates one or more potential goals, selects one or more of the potential goals, and develops one or more trajectories by which the object can achieve the one or more selected goals. The prediction systems and methods described herein can include or leverage one or more machine-learned models that assist in predicting the future locations of the objects. As an example, in some implementations, the prediction system can include a machine-learned static object classifier, a machine-learned goal scoring model, a machine-learned trajectory development model, a machine-learned ballistic quality classifier, and/or other machine-learned models. The use of machine-learned models can improve the speed, quality, and/or accuracy of the generated predictions.

Abstract: A payload joint (10) for detachably attaching to each other two adjacent construction elements (2) in a spacecraft and/or launch vehicle, the payload joint (10) comprises two opposing clamps (11a, 11b) and two opposing flanges of the construction elements collaborating with angled surfaces of the clamps (11a, 11b). The payload joint comprises a bolt that connects the clamps (11a, 11b) and drives them towards each other when tightening the payload joint (10). The payload joint (10) further comprises a bolt cutter (101) arranged for cutting the bolt upon activation.

Abstract: An apparatus for loading and deploying cargo from a motor vehicle includes a liftgate, a liftgate drive module to displace the liftgate between a closed position and an opened position, a cargo receiver carried on the liftgate and an actuator to raise and lower cargo with respect to the cargo receiver. Related methods of deploying cargo and loading cargo are also provided.

Abstract: Systems, apparatuses, and methods are provided herein for receiving aerial vehicle delivery. An apparatus for receiving aerial vehicle delivery comprises a receiving pad configured to receive a package released by an aerial vehicle; one or more accessory couplers attached to the receiving pad and configured to allow a receiving pad accessory to couple to and uncouple from the receiving pad; and a wall portion surrounding at least a portion of the receiving pad, the wall portion being removably coupled to the receiving pad via an accessory coupler.

Abstract: A fixed-wing aircraft and flight control method and system thereof are provided. The flight control method includes steps of: setting a landing site of the fixed-wing aircraft; calculating a landing runway which starts from a runway origin and ends at the landing site and is formed by alternately connecting horizontal runways with inclined runways, wherein a horizontal distance between the runway origin and the landing site is determined according to a type of the fixed-wing aircraft, and a descent rate coefficient of the inclined runways varies with a horizontal length of the inclined runways; obtaining a current location of the fixed-wing aircraft and calculating a return route which starts from the current location of the fixed-wing aircraft and ends at the runway origin; and forming a return flight line by combining the return route with the landing runway.

Abstract: A system for moving loads comprises a cargo hold floor, at least one row of rollers integrated into the floor, at least one guide rail in the floor and extending parallel to the at least one row of rollers, and a least one transport vehicle. The vehicle is received in the guide rail and movable along the guide rail and comprises at least one connecting element which is movable between first and second operating positions wherein the connecting element, in its first operating position, is arranged such that the vehicle is positionable under a load deposited onto the at least one row of rollers and, in its second operating position, is arranged such that it interacts with the load so as to connect the load to the vehicle such that the load is entrained by the vehicle when the vehicle is moved along the guide rail.

Abstract: An unmanned vehicle obtains first location information associated with a customer order, which causes the unmanned vehicle to travel to a first location. While at the first location, the unmanned vehicle receives, from another device, second location information. The unmanned vehicle uses the second location information to travel to a second location where the other device is located. Once at the second location, the unmanned vehicle performs one or more operations involved with fulfillment of the order.

Abstract: The present invention relates to an aircraft docking system comprising: a light based verification and positioning system adapted to scan a volume (120) in connection to a stand, a receiving unit adapted to receive surveillance data from an airport surveillance system, wherein the light based verification and positioning system is further adapted to control the extension of the scanned volume based on the received surveillance data.

Abstract: A transporter of an embodiment has a transporter, a detector, and a controller. The transporter holds a selected object from among a plurality of objects and transports the selected object in a first direction in a first state, and then configured to transport the selected object, while holding the selected object, in a second direction different from the first direction and not anti-parallel to the first direction, in a second state. The detector detects a change from the first state to the second state, wherein, in the second state, the transporter can transport the selected object in the second direction without disturbance by the presence of any other object than the selected object. The controller stops transporting the selected object in the first direction, in case that the detector detected the change from the first state to the second state.

Abstract: An apparatus and method of a wing fold system may include a latch assembly rotating an unfixed portion of a wing, with respect to a fixed portion of the wing, between a flight position of the wing and a folded position of the wing. A first portion of the wing may hold a rotating portion of the latch assembly. A second portion of the wing may hold a secured portion of the latch assembly. The rotating portion of the latch assembly may rotate between an open position and a closed position. A slot in the rotating portion may receive the secured portion of the latch assembly. A securing portion of the rotating portion may secure a secured portion of the latch assembly. The latch assembly may prevent rotation of the second portion when the wing may be in the flight position.