G05G11/00

System, apparatus and method for pedal control

An apparatus, method, and system for controlling motion in six degrees of freedom is described. The apparatus includes a support structure, a first pedal and a second pedal. A first set of three independent articulating mechanisms is operatively connected to the support structure and the first pedal. The first set of three independent articulating mechanisms, in combination, enable motion of the first pedal in three control axes corresponding to three discrete degrees of freedom. A second set of three independent articulating mechanisms, operatively connected to the second pedal, enable motion, in combination, in three control axes corresponding to a discrete second set of three degrees of freedom. The apparatus may also include first and second sensors configured to detect the motion of the first and second pedals.

System, apparatus and method for pedal control

An apparatus, method, and system for controlling motion in six degrees of freedom is described. The apparatus includes a support structure, a first pedal and a second pedal. A first set of three independent articulating mechanisms is operatively connected to the support structure and the first pedal. The first set of three independent articulating mechanisms, in combination, enable motion of the first pedal in three control axes corresponding to three discrete degrees of freedom. A second set of three independent articulating mechanisms, operatively connected to the second pedal, enable motion, in combination, in three control axes corresponding to a discrete second set of three degrees of freedom. The apparatus may also include first and second sensors configured to detect the motion of the first and second pedals.

THROTTLE CONTROL SYSTEM FOR AN AIRCRAFT
20190009921 · 2019-01-10 ·

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.

Control unit for a medical device
10149730 · 2018-12-11 · ·

A control unit for a medical device is provided. The control unit includes a palm interface engageable by a palm of a hand, a restraint capable of elastically deforming to apply a restraining force to the dorsum of the hand and a finger interface engageable by one or more fingers of said hand.

Multidimensional Rotary Motion Apparatus Moving a Reflective Surface and Method of Operating Same
20180275395 · 2018-09-27 ·

A motion control system for controlling an image projected from an underwater projection system in a water feature includes a chassis, a mirror support coupled to the chassis, a mirror member on the mirror support, a first drive member, and a second drive member. The mirror member is configured to reflect the image projected from the underwater projection system in the water feature. The first drive member is coupled to the chassis and configured to rotate the mirror support relative to the chassis about a first axis to move the reflected image in the water feature. The second drive member is coupled to the chassis and a fixed mount and is configured to rotate the chassis and the mirror support about a second axis to move the reflected image in the water feature.

Multidimensional Rotary Motion Apparatus Moving a Reflective Surface and Method of Operating Same
20180275395 · 2018-09-27 ·

A motion control system for controlling an image projected from an underwater projection system in a water feature includes a chassis, a mirror support coupled to the chassis, a mirror member on the mirror support, a first drive member, and a second drive member. The mirror member is configured to reflect the image projected from the underwater projection system in the water feature. The first drive member is coupled to the chassis and configured to rotate the mirror support relative to the chassis about a first axis to move the reflected image in the water feature. The second drive member is coupled to the chassis and a fixed mount and is configured to rotate the chassis and the mirror support about a second axis to move the reflected image in the water feature.

Tire Inflation Assembly
20240308479 · 2024-09-19 ·

A tire inflation assembly includes an air chuck that has a pair of outlets that has a direction of air flow which is oriented at a unique direction with respect to each other. In this way the air chuck can be attached to the valve stem at a variety of orientations to enhance employing the air chuck to inflate the tire. The air chuck includes a locking mechanism which engages the valve stem for retaining the air chuck on the valve stem. The locking mechanism is urgeable to disengage the valve stem to remove the air chuck from the valve stem. A pressure gauge is integrated into the air chuck to display the air pressure in the tire when either of the outlets is attached to the valve stem.

Stability and control augmentation system

A Stability and Command Augmentation System (SCAS) for an aircraft, the SCAS including, a first input shaft providing a first rotational input; a second input shaft providing a second rotational input; and a device for summing the first and second rotational inputs to give a rotational output for controlling an actuator. A method of operating a SCAS on an aircraft, the method including providing a pilot input order in the form of a rotating first shaft, providing an augmentation input order in the form of a rotating second shaft, summing the rotation of the pilot input order and the augmentation input order to give an output order; and using the output order to control an actuator.

Stability and control augmentation system

A Stability and Command Augmentation System (SCAS) for an aircraft, the SCAS including, a first input shaft providing a first rotational input; a second input shaft providing a second rotational input; and a device for summing the first and second rotational inputs to give a rotational output for controlling an actuator. A method of operating a SCAS on an aircraft, the method including providing a pilot input order in the form of a rotating first shaft, providing an augmentation input order in the form of a rotating second shaft, summing the rotation of the pilot input order and the augmentation input order to give an output order; and using the output order to control an actuator.

Systems and Methods for Overriding Autonomous Control of a Device
20240351681 · 2024-10-24 ·

Within examples, a system is described that includes a control lever for controlling operation of a device, a first actuator coupled to the control lever via a rod, and a resettable frangible link coupling a second actuator to the control lever via the rod. The resettable frangible link enables separation of coupling of the second actuator from the control lever based on an applied force to the rod by the first actuator.