The invention relates to an improved throttle control system for an aircraft. The throttle system includes providing friction to the throttle to maintain the position of the throttle until the pilot overcomes the friction by using force to move the throttle. The throttle is attached to and positioned about a shaft to provide rotatable movement. The invention uses a first and second friction resistance to maintain the position of the throttle along with an automatic regulating device capable of automatically controlling rotation of the shaft having a geared motor assembly.

An input device for operating a musical instrument having musical behavior of string instruments, which comprises a key plate unit containing a set of input keys to be pressed by a player, in order to generate a first set of electric input signals, which emulate a combination of pressed keys of a musical instrument or a combination of pressed strings; a stick unit with variable tension of displacement including a stick to be moved by the player between predetermined discrete positions, which emulate a combination of strummed strings of a musical instrument.

An input device for operating a musical instrument having musical behavior of string instruments, which comprises a key plate unit containing a set of input keys to be pressed by a player, in order to generate a first set of electric input signals, which emulate a combination of pressed keys of a musical instrument or a combination of pressed strings; a stick unit with variable tension of displacement including a stick to be moved by the player between predetermined discrete positions, which emulate a combination of strummed strings of a musical instrument.

A gimbal support that senses rotational displacement and provides haptic feedback in one, two or three dimensions of a manually-operated control member used to generate control inputs using a single hand while also limiting cross-coupling.

An input device, such as a joystick, has an operating device, a magnetorheological brake device, and a controller for activating the brake device. An operating lever is disposed on a supporting structure for pivoting around at least one pivot axis. The brake device is coupled with the pivot axis for controlled damping of a pivoting motion of the operating lever. The brake device has a rotary damper with two components, namely, an inside component and an outside component. The outside component radially surrounds the inside component and a damping gap is formed in between that is filled with a magnetorheological medium. The damping gap can be exposed to a magnetic field to damp a pivoting motion between the two contrapivoting components about an axis. One of the components has radial arms equipped with an electric coil whose winding extends adjacent to and spaced apart from the axis.

A joystick including a main housing with a first control surface and a second control surface. A ball rotationally engages the first control surface. A shaft has a first end that releasably engages the ball. A shoe rotationally engages the second control surface. A main spring has a first end for pressing the shoe against the second control surface. A center lock housing engages a second end of the main spring and houses a slider and a lock spring. The slider selectively permits and prevents movement of the shoe along the shaft. The lock spring presses the slider into a desired default position. A knob releasably engages the second end of the shaft. A boot covers portions of the joystick.

There is provided a transmitter for facilitating control of a flying object including an elevation control lever 22 for controlling a flight height of a helicopter 1, a cover 24 through which the elevation control lever 22 passes via an opening 26, a step 27 formed on an edge of the opening 26, and a rotation member 28, which rotates, disposed to a backside of the cover 24, where apart of the cover 24 is formed into a curved surface which overlaps a curved surface of the rotation member 28, and rotational speeds of motors 11, 12 internally mounted on the helicopter 1 are set corresponding to the step 27.

The invention relates to an improved throttle control system for an aircraft. The throttle system includes providing friction to the throttle to maintain the position of the throttle until the pilot overcomes the friction by using force to move the throttle. The throttle is attached to and positioned about a shaft to provide rotatable movement. The invention uses a first and second friction resistance to maintain the position of the throttle along with an automatic regulating device capable of automatically controlling rotation of the shaft having a geared motor assembly.

A rotary damper for damping a pivoting motion has two components, one component being an inside component and the other component an outside component. The outside component radially surrounds the inside component at least in sections. Between the components a damping gap is formed that is bordered radially inwardly by the inside component and radially outwardly, by the outside component. The gap is filled with a magnetorheological medium. The damping gap can be exposed to a magnetic field to damp a pivoting motion between the two counter-pivoting components about an axle. One of the components is provided with a plurality of radially extending arms. The arms are equipped with an electric coil having a winding, the winding extending adjacent to the axle and spaced apart from the axle.

A joystick controller is disclosed for controlling movement of a boom lift platform, the controller having actuators or the like that provide one or more forms of tactile feedback that are intuitively interpreted and adjusted by the user of the joystick motion control, the joystick being neutrally-biased to effect a null movement when the joystick is positioned in a neutral position, but also being adapted with at least one form of tactile feedback by which the joystick controller conveys information about the boom lift's operation to the joystick operator, such as through resistive force or through vibrations or the like.