Disclosed herein are embodiments of a servo-control system comprising at least one pneumatic actuator comprising a movable member, at least one proportional pneumatic valve configured to control fluid flow between the at least one pneumatic actuator and a pressurized fluid supply or a vent, a plurality of pressure sensors each configured to independently measure pressure in a respective supply line to the at least one pneumatic actuator, at least one position sensor configured to measure a position of the moveable member, and a controller. The controller is configured to determine a control signal based at least in part on pressure measurements of the plurality of pressure sensors and a position measurement of the at least one position sensor, and apply the control signal to at least one proportional pneumatic valve to move the movable member to a target position.

Various embodiments of the present disclosure provide a rotorcraft-assisted system and method for launching and retrieving a fixed-wing aircraft into and from free flight. The launch and retrieval system includes a modular multicopter, a storage and launch system, an anchor system, a flexible capture member, and an aircraft-landing structure. The multicopter is attachable to the fixed-wing aircraft to facilitate launching the fixed-wing aircraft into free, wing-borne flight. The storage and launch system is usable to store the multicopter (when disassembled) and to act as a launch mount for the fixed-wing aircraft by retaining the fixed-wing aircraft in a desired launch orientation. The anchor system is usable with the multicopter, the flexible capture member, and the aircraft-landing structure to retrieve the fixed-wing aircraft from free, wing-borne flight.

Various embodiments of the present disclosure provide a rotorcraft-assisted system and method for launching and retrieving a fixed-wing aircraft into and from free flight. The launch and retrieval system includes a modular multicopter, a storage and launch system, an anchor system, a flexible capture member, and an aircraft-landing structure. The multicopter is attachable to the fixed-wing aircraft to facilitate launching the fixed-wing aircraft into free, wing-borne flight. The storage and launch system is usable to store the multicopter (when disassembled) and to act as a launch mount for the fixed-wing aircraft by retaining the fixed-wing aircraft in a desired launch orientation. The anchor system is usable with the multicopter, the flexible capture member, and the aircraft-landing structure to retrieve the fixed-wing aircraft from free, wing-borne flight.

The invention relates to a method for operating a vibrating ram arrangement comprising a hydraulic assembly with a hydraulic pump driven by an internal combustion engine, a vibrator connected to the hydraulic assembly in a hydraulic circuit, a hydraulic clamping device connected to the vibrator for a material to be rammed, and a controller, with which a fluid flow through a hydraulic motor of the vibrator can be activated and deactivated and with which the hydraulic clamping device can be closed and opened. According to the invention, the controller requests at least one operating state value during a pause in the operation when the vibrator is deactivated and automatically stops the internal combustion engine if the operating state value corresponds to a specified value. Additionally, the controller automatically starts the internal combustion engine in order to resume the vibrating ram operation in the event of a user signal.

The invention relates to a method for operating a vibrating ram arrangement comprising a hydraulic assembly with a hydraulic pump driven by an internal combustion engine, a vibrator connected to the hydraulic assembly in a hydraulic circuit, a hydraulic clamping device connected to the vibrator for a material to be rammed, and a controller, with which a fluid flow through a hydraulic motor of the vibrator can be activated and deactivated and with which the hydraulic clamping device can be closed and opened. According to the invention, the controller requests at least one operating state value during a pause in the operation when the vibrator is deactivated and automatically stops the internal combustion engine if the operating state value corresponds to a specified value. Additionally, the controller automatically starts the internal combustion engine in order to resume the vibrating ram operation in the event of a user signal.

Disclosed herein are embodiments of a lift apparatus and systems containing a support and at least one lift apparatus for moving a substrate between the support and a transfer plane, using a servo-control system. Further disclosed herein are methods for servo control of a lift apparatus and lifting a substrate off of a support or lowering the substrate onto the support.

A system, for providing a rotary power to an implement of a machine, includes a first motor control valve associated with a first motor of the machine and a second motor control valve associated with a second motor of the machine. The first motor control valve is configured to be actuated at a first shift point to shift the first motor such that the first motor and the second motor switch between a first implement drive speed and a second implement drive speed. The second motor control valve is configured to be actuated at a second shift point to shift the second motor such that the first motor and the second motor switch between the second implement drive speed and a third implement drive speed. The first and second shift points are based on loading of the implement during operation. In addition, the first and second shift points are different.

Disclosed herein are embodiments of a servo-control system comprising at least one pneumatic actuator comprising a movable member, at least one proportional pneumatic valve configured to control fluid flow between the at least one pneumatic actuator and a pressurized fluid supply or a vent, a plurality of pressure sensors each configured to independently measure pressure in a respective supply line to the at least one pneumatic actuator, at least one position sensor configured to measure a position of the moveable member, and a controller. The controller is configured to determine a control signal based at least in part on pressure measurements of the plurality of pressure sensors and a position measurement of the at least one position sensor, and apply the control signal to at least one proportional pneumatic valve to move the movable member to a target position.

Various embodiments of the present disclosure provide a rotorcraft-assisted system and method for launching and retrieving a fixed-wing aircraft into and from free flight. The launch and retrieval system includes a modular multicopter, a storage and launch system, an anchor system, a flexible capture member, and an aircraft-landing structure. The multicopter is attachable to the fixed-wing aircraft to facilitate launching the fixed-wing aircraft into free, wing-borne flight. The storage and launch system is usable to store the multicopter (when disassembled) and to act as a launch mount for the fixed-wing aircraft by retaining the fixed-wing aircraft in a desired launch orientation. The anchor system is usable with the multicopter, the flexible capture member, and the aircraft-landing structure to retrieve the fixed-wing aircraft from free, wing-borne flight.

Various embodiments of the present disclosure provide a rotorcraft-assisted system and method for launching and retrieving a fixed-wing aircraft into and from free flight. The launch and retrieval system includes a modular multicopter, a storage and launch system, an anchor system, a flexible capture member, and an aircraft-landing structure. The multicopter is attachable to the fixed-wing aircraft to facilitate launching the fixed-wing aircraft into free, wing-borne flight. The storage and launch system is usable to store the multicopter (when disassembled) and to act as a launch mount for the fixed-wing aircraft by retaining the fixed-wing aircraft in a desired launch orientation. The anchor system is usable with the multicopter, the flexible capture member, and the aircraft-landing structure to retrieve the fixed-wing aircraft from free, wing-borne flight.