Multiple degrees of translational adjustment pedals

1. A pedal system for an aircraft comprising:

a pedal configured for manipulation through at least one operational degree of freedom by a pilot to provide control inputs to the aircraft;

a pedal mounting mechanism configured for supporting the pedal within a cockpit of the aircraft for manipulation by the pilot, the pedal mounting mechanism providing at least two adjustment degrees of freedom for adjusting the position of the pedal;

wherein the at least two adjustment degrees of freedom includes a first adjustment degree of freedom that is a rotational degree of freedom and a second adjustment degree of freedom that is a translational degree of freedom.

2. A pedal system for an aircraft comprising:

a pedal configured for manipulation to provide control inputs to the aircraft;

a pedal mounting mechanism supporting the pedal for manipulation through at least one operational degree of freedom by a pilot, the pedal mounting mechanism providing first and second adjustment degrees of freedom for adjusting the position of the pedal, the pedal mounting mechanism including:

a main support;

a pivoting support body operably coupled to the main support for rotation about a support body axis of rotation providing the first adjustment degree of freedom, the pivoting support body being operably coupled between the main support and the pedal, the pedal being operably coupled to the pivoting support body; a first actuator coupled to the pivoting support body configured for driving the pivoting support body relative to the main support about the support body axis of rotation;

the pedal being operably mounted to the pivoting support body for translational motion along the pivoting support body providing the second adjustment degree of freedom; and

a second actuator operably coupled to the pedal, the second actuator configured for translating the pedal along the pivoting support body.

3. The pedal system of claim 2 , wherein the first and second actuators are linear actuators.

4. A pedal system for an aircraft comprising:

a pedal configured for manipulation through at least one operational degree of freedom by a pilot to provide control inputs to the aircraft;

a pedal mounting mechanism configured for supporting the pedal within a cockpit of the aircraft for manipulation by the pilot, the pedal mounting mechanism providing at least two adjustment degrees of freedom for adjusting the position of the pedal;

wherein the pedal mounting mechanism includes:

a main support,

a pivoting support body operably coupled to the main support for rotation about a support body axis of rotation, the pivoting support body being operably coupled between the main support and the pedal, the pedal being operably coupled to the pivoting support body;

wherein the pedal is operably mounted to the pivoting support body for translational motion along the pivoting support body; and

further including an adjustable coupling operably coupling the pedal to the pivoting support body, the adjustable coupling providing a third adjustment degree of freedom for adjusting the position of the pedal that is a rotational degree of freedom about a pedal axis of rotation.

5. The pedal system of claim 4 , wherein the pedal axis of rotation and the support body axis of rotation are substantially parallel to one another.

6. A pedal system for use in an aircraft cockpit having a pilot seat and a flight deck floor, the pedal system comprising:

a pedal configured for manipulation through at least one operational degree of freedom by a pilot to provide control inputs to the aircraft;

a pedal mounting mechanism configured for supporting the pedal within the cockpit of the aircraft relative to the pilot seat and flight deck floor for manipulation by the pilot, the pedal mounting mechanism providing a first adjustment degree of freedom for adjusting the position of the pedal toward and away from the seat and a second adjustment degree of freedom for adjusting the position of the pedal toward and away from the flight deck floor;

wherein the pedal mounting mechanism includes:

a main support,

a pivoting support body operably coupled to the main support for rotation about a support body axis of rotation, the pivoting support body being operably coupled between the main support and the pedal, the pedal being operably coupled to the pivoting support body;

wherein the pedal is operably mounted to the pivoting support body for translational motion along the pivoting support body;

further including an adjustable coupling operably coupling the pedal to the pivoting support body, the adjustable coupling providing a third adjustment degree of freedom for adjusting the position of the pedal that is a rotational degree of freedom about a pedal axis of rotation.

7. The pedal system of claim 6 , wherein the pedal axis of rotation and the support body axis of rotation are substantially parallel to one another.

8. A pedal system for use in an aircraft cockpit having a moveable pilot seat and a flight deck floor, the pedal system comprising:

a pedal configured for manipulation through at least one operational degree of freedom by a pilot to provide control inputs to the aircraft;

a pedal mounting mechanism configured for supporting the pedal within the cockpit of the aircraft relative to the pilot seat and flight deck floor for manipulation by the pilot, the pedal mounting mechanism providing a first adjustment degree of freedom for adjusting the position of the pedal toward and away from the seat and a second adjustment degree of freedom for adjusting the position of the pedal toward and away from the flight deck floor, the pedal mounting mechanism including:

a main support,

a pivoting support body operably coupled to the main support for rotation about a support body axis of rotation, the pivoting support body being operably coupled between the main support and the pedal, the pedal being operably coupled to the pivoting support body;

a first actuator coupled to the pivoting support body configured for driving the pivoting support body relative to the main support about the support body axis of rotation;

the pedal being operably mounted to the pivoting support body for translational motion along the pivoting support body.

9. The pedal system of claim 8 , wherein one of the first and second adjustment degrees of freedom is a rotational degree of freedom and the other one of the first and second adjustment degrees of freedom is a translational degree of freedom.

10. The pedal system of claim 8 , further comprising a second actuator operably coupled to the pedal, the second actuator configured for translating the pedal along the pivoting support body.

11. The pedal system of claim 10 , wherein the first and second actuators are linear actuators.

12. The pedal system of claim 10 , further comprising a controller operably coupled to the first and second actuators, the controller configured to control the first and second actuators to drive the pedal between a pilot operational set position and a retracted position having a different position relative to the flight deck floor and the pilot seat.

13. The pedal system of claim 12 , wherein the retracted position provides increased space for the pilot to extend their legs under the pedal as compared to the pilot operational set position.