Abstract: A universal adapter system and method for coupling payloads and launch vehicles are disclosed to provide optimum payload configurability. A modular bulkhead panel may be used that can support a plurality of payload platforms such that the layout of the plurality of payload platforms on the bulkhead panel can be altered without requiring structural redesign. A carbon composite honeycomb structural frame panel may be used. Multiple bulkhead panels can be stacked to handle larger payload weights. Hollow hexagonal keyways can be used to permit cable access to and from a missile deployment module. Hexagonal payload adapter platforms may be used to join the payload to the honeycomb bulkhead panel.

Abstract: The invention relates to a cargo-hold floor for aircraft which is received on a grid structure (1). The grid structure (1) comprises essentially longitudinal members (2) and crossmembers (3). Exchangeably arranged floor plates (80), furthermore roller conveyor apparatuses (50) and lashing points (10) for the fastening of cargo articles, such as pallets, containers or vehicles, are received on the grid structure (1). Furthermore, locking units (98) are provided, which comprise lock elements (100) capable of being folded open and of being folded away. The lashing points (10) are located at the intersection points of the longitudinal members (2) and of the crossmembers (3). The roller conveyor apparatuses (50) and the locking units (98) are always located at the same installation location both in their erected position and in their countersunk drive-over and stowage position.

Abstract: An unmanned aerial vehicle (UAV) for making partial deliveries of cargo provisions includes a UAV having one or more ducted fans and a structural interconnect connecting the one or more fans to a cargo pod. The cargo pod has an outer aerodynamic shell and one or more internal drive systems for modifying a relative position of one or more cargo provisions contained within the cargo pod. Control logic is configured to, after delivery of a partial portion of the cargo provisions contained within the cargo pod, vary a position of at least a portion of the remaining cargo provisions to maintain a substantially same center of gravity of the UAV relative to a center of gravity prior to delivery of the partial portion. Other center of gravity compensation mechanisms may also be controlled by the control logic to aid in maintaining the center of gravity of the UAV.

Abstract: An aircraft elevator system includes a fixed frame, a floating frame coupled to the fixed frame, and a cabin coupled to the floating frame. The floating frame can move with respect to the fixed frame and the cabin can move with respect to the floating frame. The system can include an actuating system operating at least one pulley system to move the cabin between upper and lower positions, which respectively can be inside and outside the aircraft. In some embodiments, the system includes a support assembly that moderates or eliminates load transfer between the system and an aircraft upper deck floor structure. In some embodiments, the cabin includes a ramp configured to deploy when approaching the lower position and to retract to a stowed position when the cabin moves from the lower position toward the upper position. The ramp can include a sensor to control cabin movement.

Abstract: A releasable deployment line for a parachute system is provided. The releasable deployment line may include a first segment of material including an aircraft end configured to be operably connected to an aircraft, and a release end configured to be operably connected to a first section of a multi-ring release system. The replaceable deployment line may further include a second segment of material including a container end configured to be operably connected to a parachute container, and a ring end configured to be operably connected to a second section of the multi-ring release system and a third segment of material. The third segment of material may include a parachute end configured to be operably connected to a parachute within the parachute container, and a pin end configured to be operably connected to a retaining pin associated with the first section of the multi-ring release system.

Abstract: An aircraft comprises a cargo compartment having a cargo-compartment floor, and at least one functional unit, such as a water tank, a waste-water tank, or an electrical equipment rack. The functional unit is disposed on a pallet so that the functional unit can be transported into, and installed in, the cargo compartment. A fixation device attaches the pallet to the cargo-compartment floor.

Abstract: Aircraft decoy arrangement and method for generating a decoy signal from an aircraft having an isolated decoy. An aircraft receiver detects a threat signal from a threat source targeting the aircraft. An aircraft signal processor produces a decoy relay signal based on the threat signal, where the decoy relay signal frequency is significantly lower than the threat signal frequency and is slowly attenuated through air, the signal processor calibrating the decoy relay signal in accordance with a received test signal to compensate for inaccuracies. An aircraft transmitter transmits the decoy relay signal and an optional reference signal to the decoy, where it is received by a decoy receiver, converted back to a decoy signal by a decoy frequency converter, and transmitted by a decoy transmitter, causing the threat source to detect the decoy signal and lock onto the decoy rather than the aircraft.

Abstract: A super-transporter aircraft for transporting at least one element of a secondary aircraft, wherein the structural rigidity of a fuselage of the super-transporter is at least partly imparted by the transported element. The super-transported aircraft can be equipped with a securing device for securing the transported element to the fuselage of the super-transporter aircraft, the securing device adapted to pick up the loads to which the super-transporter aircraft is subjected.

Abstract: A system and methods for airborne launch and recovery of aircraft. In one embodiment the system comprises a flexible tether configured to be towed behind an airborne mother ship. A drag device is secured to a distal end of the flexible tether to generate drag and maintain tension in the flexible tether. A reel associated with the mother ship anchors a proximal portion of the flexible tether and selectively lets out and takes up the flexible tether to adjust a length of the flexible tether. A capture mechanism associated with the aircraft engages the flexible tether to enable the aircraft to translate along the flexible tether. In embodiments of the present methods, a flexible tether is deployed from an airborne mother ship. An aircraft translates forward and rearward along the flexible tether. Prior to launch, the weight of the aircraft is transferred from the flexible tether to the wings. During recovery, the weight of the aircraft is transferred from the wings to the flexible tether.

Abstract: A device and method for transferring cargo are disclosed, including transferring cargo between an aft-loading aircraft and a ground transportation vehicle. In one embodiment, the invention may include a tilt frame, a transfer bed, and an adjustable carriage. The tilt frame may be pivotally engaged to a vehicle chassis where the tilt frame has a first end near the cab of the vehicle and a second end distal from the cab. The transfer bed may have a first end connected to the tilt frame and may be movable along an upper surface of the tilt frame. The adjustable height carriage may support a second end of the transfer bed. The transfer bed may be leveled at varying heights by moving the first end of the transfer bed along the upper surface of the tilt frame, and by varying the height of the carriage.

Abstract: An aircraft for carrying cargo in one or more containers. The aircraft includes a fuselage structure having a plurality of nodes and a plurality of elements connecting the nodes to form a space frame in which to carry cargo. At least some of the nodes are positioned in the space frame based on dimensions of the one or more containers. The fuselage structure is more compact, lighter and less expensive compared to conventional semi-monocoque fuselages.

Abstract: A method and apparatus for a mobile tail support vehicle moving a swing tail cargo door of a swing tail aircraft. A mobile tail support apparatus is engaged to the swing tail cargo door on the swing tail aircraft. The swing tail cargo door is moved from a first position to a second position using the mobile tail support apparatus. Vertical reaction occurs to vertical loads on the swing tail cargo door during movement of the swing tail aircraft by the mobile tail support apparatus. Loads on a hinge and/or swing tail cargo door are reduced during the movement of the swing tail cargo door using the mobile tail support apparatus.

Abstract: A system for loading and unloading a cargo assembly onto and from an aircraft. The system comprises an aircraft and a movable platform. The aircraft comprises a forward fairing, an aft fairing, a spine disposed between the forward fairing and the aft fairing and a plurality of mounts coupled to the spine and configured to structurally engage the cargo container onto the spine. The aft fairing is movable between a fixed position for flight and an open position for at least loading and unloading of the cargo assembly. The aircraft is configured such that an unobstructed passageway is provided in an area underneath the spine during loading or unloading of the cargo assembly. An aft access is provided when the aft fairing is moved to the open position. The movable platform is used to maneuver the cargo assembly for loading and unloading onto and from the spine, respectively.

Abstract: A system and method for cargo handling is provided. The system includes a transport vehicle including a cargo bay capable of housing a plurality of cargo containers, and a loading dock for coupling to the cargo bay. The system also includes at least one railcar and pylons positioned along a floor of the cargo bay. A predetermined number of pylons are operable to elevate and lower a cargo container within the cargo bay. The present invention also provides a railcar for transporting cargo containers, as well as an apparatus for positioning at least one cargo container within a transport vehicle. The present invention also provides a system for aligning a loading dock and a transport vehicle that includes a mechanism for adjusting the height of the transport vehicle or loading dock, or a plurality of engagement members that are capable of aligning the loading dock and transport vehicle.

Abstract: An aircraft 1 comprises a walkway 11 moveable between a stowed position and a deployed position. The aircraft may be arranged such that the walkway, in the deployed position, defines a path, at least a portion of which extends from the fuselage at an angle, when viewed from above, of less than 90 degrees to the longitudinal axis of the aircraft. The walkway 11, in the stowed position, may be located at an angle, when viewed from above, of less than 80 degrees to the longitudinal axis of the aircraft. The opening 9 may be located in a region extending from 20% to 80% of the total cabin length. The walkway may be further moveable to a second deployed position.

Abstract: A missile includes several subvehicles that are initially mechanically coupled to a missile main body, and a separation system for separating the subvehicles form the missile main body. The separation system has a single triggering mechanism to simultaneously provide energy to separate all of the subvehicles. This advantageously provides only a single shock to the system by actuating the system to separate the subvehicles. By limiting the shocks to the single shock of actuating the energy system and the shocks of the mechanical disengagement of the individual subvehicles, the disengagement system has improved performance. The subvehicles may be separated from the main body in radial directions substantially perpendicular to a central axis of the main body. This may provide for smoother disengagement, with less tipping, and may provide for greater, more uniform spacing between the disengaged subvehicles.

Abstract: An apparatus for controlling the environment of an internal airplane space during loading and unloading of cargo, a cargo tent for use in such transfers and a method of transfer. A collapsible cargo tent is located on a cargo transfer platform at one end of a mobile cargo lift. The collapsible cargo tent may include a collapsible frame and a cargo loader thermal curtain with a vertical strip curtain in an opening at either end. Also, the cargo tent may include a conformable flexible shield at strip curtain opening. The conformable flexible shield engages the fuselage at the door of an aircraft to form an environmental seal and the cargo loader thermal curtain forms a thermal air lock at the door such that cargo may pass through the airlock with the door open and without exposing the cargo bay to external environment.

Abstract: A roll-on/roll-off, aircraft-borne sensor pod deployment system having an operator station and a sensor pallet system and method of using same. The operator station has a base platform, a shelter box mounted on the base platform for accommodating a human operator, and a computer installed inside the shelter box. The sensor pallet system has a base platform, a linear system mounted on the base platform, a rotational system mounted on the linear system, a mechanical arm attached to the rotational system, a sensor pod attached to the mechanical arm, and an electrical control system that provides power to the deployment system and controls movements of the sensor pallet system. In operation, the sensor pod can be retracted into a compact, stowing position, or extended out an opening in the aircraft for an unobstructed field of view. The deployment system optionally includes an apparatus and method for sealing the aircraft opening.

Abstract: The present invention relates to a system for transportation of goods in a loading space. The system comprises a conveyor (1) for goods which is drivable to and for in the loading space.

Abstract: A floor module with roller conveyors which define an aircraft cargo hold floor with a loading level is provided. The floor modules have cross-members to which the roller conveyor is attached. A rail with two side pieces is provided, between which rollers are rotatably mounted in such a way that they protrude above upper edges of the rails. The side pieces are joined to one another by a floor section. To improve the strength of the floor module, the floor section has a bent region inclined in cross-section at an angle to the loading level, the bent region dividing the floor section into one partial section lying higher and one partial section lying lower relative to the upper edges.

Abstract: A transfer of ordnance units from a first aerial vehicle to a second aerial vehicle performed while both vehicles are airborne. The first aircraft is used as an ordnance storage, ordnance delivery and ordnance supplier platform. The second aircraft has the functionality and capability of delivering the received ordnance to designated targets. The first aircraft includes an ordnance storage apparatus, an ordnance transfer assembly, a computer-based highly accurate ordnance transfer control apparatus, and an ordnance transfer apparatus operating crew. The ordnance transfer assembly establishes temporarily a transfer link between the aircraft and utilizes an ordnance conveyor mechanism for the delivery of the ordnance units. The second aircraft includes a multi-use multi-purpose pylon that receives the transferred ordnance in the proper manner. The aircrafts can be uninhabited.

Abstract: An aircraft hold including a floor having a substantially flat central part and a side part disposed along each longitudinal edge of the central part and inclined in relation thereto. The aircraft hold also includes at least one bench with a seat that can move between a position in which it is substantially parallel to the central part of the floor and a position in which it is folded against a wall of the hold.

Abstract: The system and apparatus of the present invention is generally comprised of a non-dedicated, temporarily installed, airborne special mission payload mounting system which is mechanically interfaced to the Air Deployment System (ADS) rails of a host cargo aircraft. Where a host aircraft does not possess ADS rails, an Adaptive ADS rail section typical of those used by the host aircraft, is installed to the existing cargo floor “D” rings using adjustable cam locks familiar to those skilled in the art of aircraft cargo restraint systems. Where the host aircraft does not have the required cargo “D” rings installed they are then temporarily installed within the “D” ring bolt sockets to enable the aircraft to accommodate mounting of the Adaptive ADS rail section plate.

Abstract: An unmanned aerial vehicle (UAV) has a payload or body affixed at one end of an elongated airfoil. The entire airfoil/payload combination rotates about a center of mass to define a rotor disk. Thrust is provided by air-augmented rocket engine thrusting tangentially at a location remote from the payload. A control system maintains knowledge of its environment, as by a camera, to produce directional control signals which actuate lift control means in synchronism with the rotational position of the vehicle. A deployable object may be carried. Protection of the stowed vehicle is provided by blister packaging.

Abstract: The invention relates to a device for moving objects, particularly luggage, in an aircraft hold, said device including a moving wall (10) and at least one belt. One end of the belt (20) is connected to a roller (24) around which the belt (20) is wound. The other end of the belt (20) is attached to the moving wall (10). A lower section of the belt (20) extends from the moving wall (10) to a threshold element (22) and an upper section of the belt (20) extends from the threshold element (22) to the moving wall (10).

Abstract: A device for locking containers into place includes a frame, at least one locking claw affixed to the frame, and an adjustment component which is affixed to the locking claw. A position of a container to be locked into place is adjustable relative to the locking claw in a longitudinal direction of the frame.

Abstract: A device intended for a hold that can receive containers and luggage simultaneously. The hold includes a freight loading system including rollers defining a rolling surface on which a container can move with the movement of the rollers. The device includes a unit including conveyor belts disposed longitudinally in the hold one after the other such as to extend over at least part of the length of the hold. Each conveyor belt includes an upper section configured to receive an object to be moved and each conveyor belt can move between a first raised position in which the upper section of the belt is located above the rolling surface defined by the rollers of the freight loading system and a second position in which the upper section of the belt is located below the rolling surface.

Abstract: A payload or cargo is delivered from a cargo hold of an aircraft during flight, by orienting the fuselage into a nose-up and tail-down position of at least 30 degrees off horizontal, and lowering the cargo from a cargo hold in the fuselage by means of one or more lines. Preferred vertical takeoff and landing (VTOL) aircraft include tilt-rotor or tilt-wing aircraft, and especially preferred aircraft are capable of generating control moments with their rotors to assist in orientating the fuselage of the aircraft into a nose-up and tail-down position.

Abstract: In one embodiment, a method of operating an aircraft having a passenger cabin and a cargo hold, comprises the steps of directing passengers to board the aircraft, directing passengers to deposit their luggage in a luggage deposit location on-board the aircraft, and subsequently taking the deposited luggage from the luggage deposit location and then storing the luggage in the cargo hold of the aircraft. In another embodiment, a method of unloading an aircraft having a cargo hold and a passenger cabin, comprises the steps of transporting items of luggage from the cargo hold to a luggage collection location on-board the aircraft, and directing passengers to collect their luggage from the luggage collection location and to disembark the aircraft is also provided. Information may be gathered with regard to the identity of passengers embarking and disembarking the aircraft. Yet another embodiment relates to an aircraft having a passenger cabin, a cargo hold, and a luggage handling system mounted in the cargo hold.

Abstract: A system for in-air deployment of objects utilizes an aircraft having a hatch that can be opened while the aircraft is in mid-flight. An air and pressure tight container stowed within the aircraft has a doorway that is sealed to and about the hatch from within the aircraft. Mounted within the container is an expulsion system for expelling objects from the container through its doorway and the aircraft's hatch. The container may be coupled and sealed to other containers to define a contiguous volume for storing the objects and allowing movement of the objects between containers.

Abstract: A self-adjusting loading guide and restraint for guiding and restraining aircraft unit load devices includes a base and an arm substantially upwardly extending from the base. The arm includes a vertical restraint portion and guide member having at least one substantially planar guide surface that is pivotally connected to the arm, and is movable between a first guide position and a second guide position. When the vertical restraint portion is engaged with a stowed first unit load device, the guide member assists in guiding a second unit load device away from the first unit load device and the loading guide and restraint and into a stowage location that is adjacent to the first unit load device.

Abstract: The present invention provides a method and apparatus for transporting a motorized vehicle, such as a wheelchair, between the loading bridge and cargo bin of an aircraft in a timely manner. According to one embodiment of the invention, a metal cage assembly is implemented with a drop down ramp at the front and an adjustable floor that is raised by a lever handle on either side, outside of the frame. The assembly can be attached to an end of aircraft cargo belt loader by a strap that is wrapped around the belt frame and tightened via a ratcheting clamp. The adjustable floor can be raised or lowered at one end to offset the angle of the belt loader when it is raised to an upright position, for example, to reach a galley door of an aircraft. Angling of the adjustable floor can allow the floor to be substantially parallel to the loading bridge or aircraft cargo bin, thereby enabling the easy transfer of a motorized wheelchair to and from various compartments of the aircraft.

Abstract: A roll-on/roll-off, aircraft-borne sensor pod deployment system having an operator station and a sensor pallet system and method of using same. The operator station has a base platform, a shelter box mounted on the base platform for accommodating a human operator, and a computer installed inside the shelter box. The sensor pallet system has a base platform, a linear system mounted on the base platform, a rotational system mounted on the linear system, a mechanical arm attached to the rotational system, a sensor pod attached to the mechanical arm, and an electrical control system that provides power to the deployment system and controls movements of the sensor pallet system. In operation, the sensor pod can be retracted into a compact, stowing position, or extended out an opening in the aircraft for an unobstructed field of view. The deployment system optionally includes an apparatus and method for sealing the aircraft opening.

Abstract: An aircraft capable of hovering, and having a fuselage defining an access opening; driving means for operating a rescue cradle; and a first wall movable between a closed position engaging a first portion of the opening, and a first open position allowing access to the first portion of the opening. The aircraft has a member connected functionally to the first wall and in turn having at least one flat surface; and the member is movable with respect to the wall into a first position, in which the flat surface defines a supporting surface for the cradle when the first wall is in the first open position.

Abstract: An aircraft for carrying at least one rigid cargo container includes a beam structure with a forward fuselage attached to the forward end of the beam structure and an empennage attached to the rearward end of the beam structure. Wings and engines are mounted relative to the beam structure and a fairing creates a cargo bay able to receive standard sized intermodal cargo containers. Intermodal cargo containers of light construction and rigid structure are positioned within the cargo bay and securely mounted therein. The beam structure is designed to support flight, takeoffs and landings when the aircraft is empty but requires the added strength of the containers securely mounted to the beam structure when the aircraft is loaded. The aircraft is contemplated to be a drone.

Abstract: A method and apparatus for aligning a swing tail cargo door. An alignment system comprises an alignment ramp, a set of pull-in hook mechanisms, and a set of lock trains. The alignment ramp may be configured for initial alignment between a swing tail cargo door and an aircraft fuselage during closing of the swing tail cargo door. The set of pull-in hook mechanisms may be disposed along an interface between the swing tail cargo door and the aircraft fuselage and may be capable of a final alignment between the swing tail cargo door and the aircraft fuselage during the closing of the swing tail cargo door. The set of lock trains may be disposed along the interface and may be capable of locking a plurality of latch actuators in the latched position.

Abstract: An air cargo power drive unit has a motor, at least one driver roller element coupled to said motor, a light source, a light detector, and a processor having memory associated therewith, said memory storing instructions. The device is configured to emit light from the light source, receive reflected light from the light detector when an air cargo is overhead, and convert the detected light into a time series of a digital samples representing a time-varying intensity of the received light. The processor then performs calculations on the digital samples to determine whether the unit load device is moving. This determination may be based, for instance, on spikes among the digital samples, and/or on first, second, or even higher-order, statistics of the detected samples.

Abstract: The present invention provides a method for loading equipment into a deployment apparatus and particularly for loading equipment in an aircraft for deployment. The method includes steps for moving a container towards the deployment apparatus in a non-upright orientation, engaging the container with the deployment apparatus, and then moving the container towards an upright orientation.

Abstract: An aerial delivery system is configured to allow delivery of one or more releasable items after the system is extracted from an aircraft. One or more linear guidance devices and releasable securing mechanisms allow the aerial delivery system to deploy one or more releasable items at an appropriate time. The one or more releasable items may be deployed simultaneously, or in a staged or staggered fashion. Through use of drag or lift-producing devices, the system may be recovered and reused. The attitude and/or azimuth orientation of the system may be varied prior to, during, and/or after release of a releasable item.

Abstract: A servicing bridge (14) for an airport (13) includes multiple servicing levels (82, 102). A bridge (81) includes one or more of the servicing levels (82, 102) and extends from a terminal of the airport (13). A ground support service sub-system is coupled to the servicing levels (82, 102) and is configured to mate with a service opening (26) of the aircraft (12). The ground support service sub-system provides services to the aircraft (12) through the service opening (26) and on the servicing levels (82, 102).

Abstract: A tilarm system for an aircraft having a nose landing gear (NLG) includes a sensor having first and second parts respectively disposed on first and second portions of the NLG that are respectively fixed to the aircraft and moveable relative to the fixed portion and operable to detect the position of the first and second portions relative to each other and to produce a tip alarm signal when the first and second NLG portions are disposed at a selected position relative to each other corresponding to an imminent aircraft tipping condition and thereby prevent the aircraft from tipping back onto the ground due to improper loading of the aircraft.

Abstract: A loading device 1 for loading and unloading of a cargo hold having at least one conveying system for positioning cargo units in the area of a floor space of the cargo hold, and with at least one guiding element guiding the conveying, and a movement aid in the area of the floor space 11 of the cargo hold 5 enabling rotation and movement of the cargo unit. Sensors detect the presence of a cargo unit in the area of the conveying system without contact the position of a cargo unit on the floor space is determined in at least two spatial dimensions without contact. The sensors make it possible to control rotating movements of the cargo units in the area of the respective conveying systems by a controller.

Abstract: A terminal (14) for an airport (13) includes multiple servicing levels (82, 102). A ground support service sub-system is coupled to the servicing levels (82, 102) and is configured to mate with a service opening (26) of the aircraft (12). The ground support service sub-system provides services to the aircraft (12) through the service opening (26) and on the servicing levels (82, 102).

Abstract: A system and method of constructing a system for delivering cargo by airdrop are provided. In short, the system uses rotor blades to slow the descent of cargo dropped from an aircraft. In one example of one embodiment, a frame is secured to a cargo pallet and at least one rotor blade is secured to the frame. The rotor blade is secured to the frame in a position such that it causes the cargo pallet and the frame to rotate in air when dropped from an elevation. In another embodiment, the rotor blade may be extendable and extend during flight.

Abstract: A mobile ground servicing unit (470) includes a stand-alone support structure (471). Wheels (473) are coupled to the support structure (471). The support structure (471) has one or more servicing levels (472, 474) that are associated with services. A ground support service sub-system is coupled to the servicing levels and is configured to mate with a service opening (26?) of an aircraft (12??). The ground support service sub-system provides the services to the aircraft (12??) through the service opening (26?) and on the servicing levels (472, 474).

Abstract: A baggage accommodation device for an aircraft, which device comprises a plurality of first rollers and a container, wherein the container comprises a base plate. The plurality of first rollers are arranged on the base plate, and the baggage accommodation device is designed such that it is sufficiently stable for said baggage accommodation device to be able to be moved into and out of the aircraft.

Abstract: An aircraft (12) includes a servicing opening (26) and multiple service levels (82, 102). The service levels (82, 102) include a noncargo-based service level (82). The service levels (82, 102) are accessible through the service opening (26). An aircraft onboard primary servicing system (66) includes a primary service sub-system (151). An aircraft primary service coupler (154) is configured to attach to a corresponding terminal primary service coupler (152). The aircraft primary service coupler (154) and the terminal primary service coupler (152) providing at least one primary service therethrough.

Abstract: Apparatus (20) for aerial transport includes a cabin (24) for containing a load and one or more cables (30), attached so as to suspend the cabin below a hovering aircraft (22). An elevator mechanism (32) is coupled to raise and lower the cabin on the one or more cables. A control unit (56) is coupled to receive an input from at least one cabin sensor (38, 40, 48, 50, 60, 62) that is indicative of the disposition of the cabin relative to the terrestrial target (26), and to control the elevator mechanism responsively to the input so as to bring the cabin into with a predetermined position relative to the terrestrial target while the aircraft is hovering.

Abstract: An air cargo loading system also includes a controller, a main control panel and a plurality of PDUs (PDUs), at least the controller and the PDUs being connected by a wired network. Each PDU has a motor, at least one driver roller element coupled to said motor, a light source, a light detector, and a processor. The light detector of each PDU is configured to receive and process an incoming coded light signal from a wireless remote control handset. The PDU's processor determines whether the received coded light signal is a valid command signal and, if so, provides a command information signal to the controller via the wired network. The controller decodes the command information signal and, in view of its knowledge of container locations, various switch settings and other status information, the controller then sends the appropriate control signals to turn on the required PDUs in response thereto.

Abstract: An air cargo loading system also includes a controller, a main control panel and a plurality of PDUs (PDUs), at least the controller and the PDUs being connected by a wired network. Each PDU has a motor, at least one driver roller element coupled to said motor, a light source, a light detector, and a processor. The light detector of each PDU is configured to receive and process an incoming coded light signal from a wireless remote control handset. The PDU's processor determines whether the received coded light signal is a valid command signal and, if so, provides a command information signal to the controller via the wired network. The controller decodes the command information signal and, in view of its knowledge of container locations, various switch settings and other status information, the controller then sends the appropriate control signals to turn, on the required PDUs in response thereto.