Rotation mechanism with sliding joint
Rotation mechanisms for rotating a payload in two, first and second degrees of freedom (DOF), comprising a static base, a first rotation arm coupled mechanically to the static base through a first rotation joint and used for rotating the payload relative to the static base around a first rotation axis that passes through the first rotation joint, a second rotation arm coupled mechanically to the static base through a second rotation joint and used for rotating the payload relative to the static base around a second rotation axis that passes through the second rotation joint, and a follower member rigidly coupled to the payload and arranged to keep a constant distance from the second rotation arm, wherein the rotation of the first arm rotates the payload around the first DOF and the rotation of the second arm rotate the payload around the second DOF.
1. A rotation mechanism for rotating a payload in two, first and second degrees of freedom (DOF), comprising:
a) a static base;
b) a first rotation arm coupled mechanically to the static base through a first rotation joint and used for rotating the payload relative to the static base around a first rotation axis that passes through the first rotation joint;
c) a second rotation arm coupled mechanically to the static base through a second rotation joint and used for rotating the payload relative to the static base around a second rotation axis that passes through the second rotation joint; and
d) a follower member rigidly coupled to the payload and arranged to keep a constant distance from the second rotation arm,
wherein the rotation of the first arm rotates the payload around the first DOF and wherein the rotation of the second arm rotates the payload around the second DOF.
2. The rotation mechanism of claim 1 , wherein the payload is coupled mechanically to the first rotation arm through an inner rotation joint.
3. The rotation mechanism of claim 1 , further comprising a first motor for rotating the payload relative to the static base around the first rotation axis and a second motor for rotating the payload relative to the static base around the second rotation axis, wherein the first and second motors are rigidly attached to the static base.
4. The rotation mechanism of claim 1 , wherein the follower member is a magnetic member separated from the second rotation arm by a constant air-gap.
5. The rotation mechanism of claim 2 , further comprising a first motor for rotating the payload relative to the static base around the first rotation axis and a second motor for rotating the payload relative to the static base around the second rotation axis, wherein the first and second motors are rigidly attached to the static base.
6. The rotation mechanism of claim 2 , wherein the follower member is a magnetic member separated from the second rotation arm by a constant air-gap.
7. The rotation mechanism of claim 3 , wherein the follower member is a magnetic member separated from the second rotation arm by a constant air-gap.
8. The rotation mechanism of claim 1 , wherein the second rotation arm includes a ring section centered around the first rotation axis.
9. The rotation mechanism of claim 1 , further comprising at least one sensing mechanism for determining a position of the payload.
10. The rotation mechanism of claim 9 , wherein the at least one sensing mechanism comprises at least one pair of a magnet and a Hall sensor.
11. The rotation mechanism of claim 9 , wherein the at least one sensing mechanism is operable to determine a position of the payload relative to the static base in the first and second DOFs.
12. The rotation mechanism of claim 10 , wherein the at least one pair of a magnet and a Hall sensor comprises a first pair of a magnet and a Hall sensor that allows determination of a rotation of the payload around the first DOF, and a second pair of a magnet and a Hall sensor that allows determination of a rotation of the payload around the second DOF.
13. The rotation mechanism of claim 11 , wherein the determinations of the position of the payload relative to the static base in the two DOFs are decoupled from each other.