Abstract: An aircrew automation system may comprise an actuation system and a computer system having a processor and one or more interfaces. The computer system can be communicatively coupled with a flight control system of an aircraft and configured to generate control commands based at least in part on flight situation data. The actuation system is operatively coupled with the computer system and comprises a robotic arm, a force sensor, and a controller. The robotic arm can be configured to engage a cockpit instrument among a plurality of cockpit instruments. The force sensor is operably coupled to the robotic arm and configured to measure a force when the robotic arm makes contact with the cockpit instrument. The controller is operably coupled with the robotic arm and the force sensor.

Abstract: A vehicle includes a fuselage having a longitudinal axis and a propulsion system that is coupled to the fuselage. The vehicle also includes a pair of articulated appendages that is coupled to the fuselage. Each one of the articulated appendages includes a plurality of airfoil segments and is moveable between a ground configuration, in which each one of the pair of articulated appendages supports the vehicle during takeoff or landing of the vehicle, and a flight configuration, in which each one of the pair of articulated appendages produces lift during flight of the vehicle.

Abstract: A workpiece manipulation system to provide high-precision manipulation of a workpiece by an aircraft. The workpiece manipulation system comprises a lifting mechanism to couple with the aircraft, an end-effector, and a processor. The lifting mechanism includes one or more joint actuators to extend or retract the lifting mechanism relative to the aircraft. The end-effector includes an end-effector actuator to control an operation of the end-effector to manipulate the workpiece. The processor is communicatively coupled with the aircraft processor and configured to control operation of the end-effector actuator and the one or more joint actuators. In operation, the processor provides feedback to the aircraft.

Abstract: Disclosed herein are aircraft and landing gear systems configured to fix an aircraft to the ground. For example, the aircraft and aircraft systems configured for ground manipulation. In one aspect, an aircraft with an arm and end-effector may be fixed a ground surface to facilitate ground-based robotic manipulation tasks.

Abstract: A method of operating a manipulation system of the type having a movable arm with a proximal end connected to a base and a distal end that is movable relative to the base and is coupled to an end-effector. The method comprises moving the distal end of the movable arm towards a target object and into contact with a stabilization object proximate to the target object, maintaining contact between the distal end of the movable arm and the stabilization object while operating the end-effector to perform a desired operation at the target object, and upon completing the desired operation at the target object, disengaging the distal end of the movable arm from contact with the stabilization object.

Abstract: An actuation system to manipulate an interface in an aircraft having an actuation controller, a vision system, a robotic arm, and a housing. Each of the vision system and the robotic arm assembly may be operatively coupled to the actuation controller. The vision system may be configured to optically image a display device of the preexisting interface, while the robotic arm assembly may be configured to engage a user-actuable device of the preexisting interface. The housing can be configured to affix to a surface adjacent the preexisting interface, where each of the vision system and the robotic arm assembly are coupled to the housing. In operation, the actuation controller may be configured to instruct the robotic arm assembly based at least in part on data from the vision system.

Abstract: An aircrew automation system that provides a pilot with high-fidelity knowledge of the aircraft's physical state, and notifies that pilot of any deviations in expected state based on predictive models. The aircrew automation may be provided as a non-invasive ride-along aircrew automation system that perceives the state of the aircraft through visual techniques, derives the aircraft state vector and other aircraft information, and communicates any deviations from expected aircraft state to the pilot. The aircrew automation may also monitor pilot health and, when needed, function as a robotic co-pilot to perform emergency descent and landing operations.

Abstract: An aircrew automation system may comprise an actuation system and a computer system having a processor and one or more interfaces. The computer system can be communicatively coupled with a flight control system of an aircraft and configured to generate control commands based at least in part on flight situation data. The actuation system is operatively coupled with the computer system and comprises a robotic arm, a force sensor, and a controller. The robotic arm can be configured to engage a cockpit instrument among a plurality of cockpit instruments. The force sensor is operably coupled to the robotic arm and configured to measure a force when the robotic arm makes contact with the cockpit instrument. The controller is operably coupled with the robotic arm and the force sensor.

Abstract: A device to determine integrity of a surface includes an exterior housing to contain and protect a plurality of components. The components include an accelerometer to measure a change in acceleration of the device, a microcontroller to monitor measurement data from the accelerometer and determine the integrity of the surface based on the measurement data. A communication circuit transmits or displays information regarding the integrity of the surface from microcontroller. A battery powers the plurality of components.

Abstract: A workpiece manipulation system is disclosed. The workpiece manipulation system is configured to provide high-precision manipulation of a workpiece by an aircraft. The workpiece manipulation system comprises a lifting mechanism to couple with the aircraft, an end-effector, and a processor. The lifting mechanism includes one or more joint actuators to extend or retract the lifting mechanism relative to the aircraft. The end-effector includes an end-effector actuator to control an operation of the end-effector to manipulate the workpiece. The processor is communicatively coupled with an aircraft processor and configured to control operation of the end-effector actuator and the one or more joint actuators.

Abstract: A robot system having a robot with a jamming gripper is disclosed. The jamming gripper may comprise granular material within a deformable membrane configured to phase transition between a malleable state and a rigid state upon modification of its internal pressure. The phase transition of the gripper may allow the robot to engage and/or grasp a target object by conforming to the shape of the target object while in its malleable state, then transitioning to its rigid state in order to firmly grasp the object. In some situations, the robot may be configured to select and/or engage a stencil before engaging the target object, so as to pre-shape the gripper before engagement with the target object.

Abstract: The present disclosure is directed to systems and methods for enabling unmanned and optionally-manned cargo delivery to personnel on the ground. For example, an aircraft may be used to provide rapid response cargo delivery to widely separated small units in demanding and unpredictable conditions that pose unacceptable risks to both ground resupply personnel and aircrew. Together with a ground vehicle, packages from the aircraft may be deployed to ground personnel in disbursed operating locations without exposing the ground personnel to the aircraft's open landing zone.

Abstract: A vehicle includes a fuselage having a longitudinal axis and a propulsion system that is coupled to the fuselage. The vehicle also includes a pair of articulated appendages that is coupled to the fuselage. Each one of the articulated appendages includes a plurality of airfoil segments and is moveable between a ground configuration, in which each one of the pair of articulated appendages supports the vehicle during takeoff or landing of the vehicle, and a flight configuration, in which each one of the pair of articulated appendages produces lift during flight of the vehicle.

Abstract: An aircrew automation system relates to the field of flight control systems, methods, and apparatuses; even more particularly, to a system, method, and apparatus for providing aircraft state monitoring and/or an automated aircrew employing a robotic arm with integrated imaging and force sensing modalities.

Abstract: A device to determine integrity of a surface includes an exterior housing to contain and protect a plurality of components. The components include an accelerometer to measure a change in acceleration of the device, a microcontroller to monitor measurement data from the accelerometer and determine the integrity of the surface based on the measurement data. A communication circuit transmits or displays information regarding the integrity of the surface from microcontroller. A battery powers the plurality of components.

Abstract: A cutting machine for detecting a defect during a manufacturing process is disclosed. The cutting machine comprises a base structure having a planar surface defining a working area, a rack to support a material spool, a cutter assembly, and a material-inspection system. The rack may be positioned at an end of the base structure to facilitate unrolling of a composite material sheet from the material spool and onto the working area. The cutter assembly comprises a cutter tool to cut the composite material sheet on the working area. The cutter assembly may be configured to move relative to the working area via a two-axis gantry. The material-inspection system comprises a plurality of non-contact ultrasonic sensors to measure one or more material properties of the composite material sheet. The measured one or more material properties can be used to detect and predict defects in the composite material sheet.

Abstract: A method of operating a manipulation system of the type having a movable arm with a proximal end connected to a base and a distal end that is movable relative to the base and is coupled to an end-effector. The method comprises moving the distal end of the movable arm towards a target object and into contact with a stabilization object proximate to the target object, maintaining contact between the distal end of the movable arm and the stabilization object while operating the end-effector to perform a desired operation at the target object, and upon completing the desired operation at the target object, disengaging the distal end of the movable arm from contact with the stabilization object.

Abstract: A workpiece manipulation system is disclosed. The workpiece manipulation system is configured to provide high-precision manipulation of a workpiece by an aircraft. The workpiece manipulation system comprises a lifting mechanism to couple with the aircraft, an end-effector, and a processor. The lifting mechanism includes one or more joint actuators to extend or retract the lifting mechanism relative to the aircraft. The end-effector includes an end-effector actuator to control an operation of the end-effector to manipulate the workpiece. The processor is communicatively coupled with an aircraft processor and configured to control operation of the end-effector actuator and the one or more joint actuators.

Abstract: An actuation system to manipulate an interface in an aircraft having an actuation controller, a vision system, a robotic arm, and a housing. Each of the vision system and the robotic arm assembly may be operatively coupled to the actuation controller. The vision system may be configured to optically image a display device of the preexisting interface, while the robotic arm assembly may be configured to engage a user-actuable device of the preexisting interface. The housing can be configured to affix to a surface adjacent the preexisting interface, where each of the vision system and the robotic arm assembly are coupled to the housing. In operation, the actuation controller may be configured to instruct the robotic arm assembly based at least in part on data from the vision system.

Abstract: A robot system having a robot with a jamming gripper is disclosed. The jamming gripper may comprise granular material within a deformable membrane configured to phase transition between a malleable state and a rigid state upon modification of its internal pressure. The phase transition of the gripper may allow the robot to engage and/or grasp a target object by conforming to the shape of the target object while in its malleable state, then transitioning to its rigid state in order to firmly grasp the object. In some situations, the robot may be configured to select and/or engage a stencil before engaging the target object, so as to pre-shape the gripper before engagement with the target object.