A robotic surgical system includes a surgical instrument and a processor. The surgical instrument includes an elongate hollow shaft having a flexible section, a sensor apparatus configured to generate sensor data about the flexible section, and a force transmission mechanism coupled to the proximal end of the shaft. The processor is communicatively coupled to the sensor apparatus. The processor is configured to receive the sensor data about the flexible section from the sensor apparatus and to combine the sensor data received from the sensor apparatus with known information regarding mechanical and material property data for the surgical instrument to derive at least one of an internal actuation force applied by the force transmission mechanism or external force information for the surgical instrument.

An object is prevented from being sandwiched between robot arms without the occurrence of unintentional operating restrictions of the robot arms. Provided is a robot system including: a robot body that is provided with at least two links that are relatively moved by at least one joint; a sensor that detects the distances from mutually opposed surfaces of the at least two links to an object inserted between the surfaces; and a control unit that performs an interference avoidance operation if the distances detected by the sensor are less than a predetermined threshold.

A robot arm having a weight compensation mechanism. In one configuration, the robot arm includes a first link which is pivotably disposed, a first auxiliary link disposed parallel to the first link, a first pulley mounted on the first auxiliary link, a second pulley mounted on the first link, a wire connecting the first pulley to the second pulley, and an elastic member having one side mounted on the first link and the other side connected to the wire to provide an elastic force to compensate for the load of the first link.

A sensor includes a first support portion, a second support portion, an incremental encoder, a magnetic-flux generating source, and a magnetoelectric transducer. The incremental encoder includes a scale supported by the first support portion and a head supported by the second support portion. The magnetic-flux generating source is supported by one of the first support portion and the second support portion. The magnetoelectric transducer is supported by another of the first support portion and the second support portion.

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.

Medical, surgical, and/or robotic devices and systems often including offset remote center parallelogram manipulator linkage assemblies which constrains a position of a surgical instrument during minimally invasive robotic surgery are disclosed. The improved remote center manipulator linkage assembly advantageously enhances the range of instrument motion while at the same time reduces the overall complexity, size, and physical weight of the robotic surgical system.

A submersible robot includes a re-configurable body transformable between at least a first configuration and a second configuration such that the re-configurable body, in the first configuration, has a hydrodynamic shape configured for efficient travel in a subsea environment, and such that the re-configurable body, in the second configuration, has a shape configured for performing a robotic task in the subsea environment.

A spacecraft includes at least one deployable propulsion module, the propulsion module including at least one thruster fixedly disposed with respect to the propulsion module, a first arrangement for coupling the propulsion module to a first portion of the spacecraft in a first configuration and a second arrangement for coupling the propulsion module to a second portion of the spacecraft in a second configuration. The spacecraft is reconfigurable, on-orbit, from the first configuration to the second configuration. In the first configuration, the deployable propulsion module is detached from the second arrangement and the at least one thruster is oriented to produce thrust in a first direction. In the second configuration, the deployable propulsion module is detached from the first arrangement and the at least one thruster is oriented to produce thrust in a second direction, the second direction being substantially different from the first direction.

A substrate processing apparatus including a frame, a first SCARA arm connected to the frame, including an end effector, configured to extend and retract along a first radial axis; a second SCARA arm connected to the frame, including an end effector, configured to extend and retract along a second radial axis, the SCARA arms having a common shoulder axis of rotation; and a drive section coupled to the SCARA arms is configured to independently extend each SCARA arm along a respective radial axis and rotate each SCARA arm about the common shoulder axis of rotation where the first radial axis is angled relative to the second radial axis and the end effector of a respective arm is aligned with a respective radial axis, wherein each end effector is configured to hold at least one substrate and the end effectors are located on a common transfer plane.

A robotic dolly transfer system configured to transport dollies includes a full dolly transfer system and an empty dolly transfer system. The full dolly transfer system and the empty dolly transfer system individually include a rail assembly and a carriage. The carriage is slidably attached to the rail assembly and includes a bottom surface that has a post extending outwardly. The rail assembly includes a rail actuator assembly having an actuator and a receiver attached to the actuator. The receiver includes an opening that receives the post such that the post floats within the opening to permit the carriage to move a predetermined amount independent from the receiver. The actuator is configured to displace the receiver such that receiver contacts the post to slide the carriage with respect to the rail assembly. A end effector is pivotally connected to a transfer arm assembly and is configured to engage the dolly.