Claims
- 1. A two-axis angular effector, comprising:
- i) a first link, comprising a first link near mounting locus and a first link far mounting locus;
- ii) a second link, comprising a second link near mounting locus and a second link far mounting locus;
- iii) a two-axis Cardan-type joint, comprising a yoke, a first set of arms connecting to the first link near mounting locus, a second set of arms connecting to the second link near mounting locus, and a first and second set of rotational shafts, said first and second rotational shafts respectively defining a first and a second rotational axis, said rotational axes defining in turn a first and second set of leverage points located such that a force applied parallel to the first (second) link produces a rotational torque about the first and second rotational axes, respectively;
- iv) a set of at least one first link linear actuator assembly, each comprising a linear activator, a first joint connected to a member of the first set of leverage points of the two-axis Cardan-type joint and a second joint connected to the first link far mounting locus, said joints contrived so that the action of each said linear activator varies the distance between the corresponding first and second joints, and so that said joints allow free relative rotation of the first and second links about the first rotational axis;
- v) a set of at least one second link linear actuator assembly, each comprising a linear activator, a third joint connected to a member of the second set of leverage points of the two-axis Cardan-type joint and a fourth joint connected to the second link far mounting locus, said joints contrived so that the action of each said linear activator varies the distance between the corresponding third and fourth joints, and so that said joints allow free relative rotation of the first and second links about the second rotational axis;
- vi) a power source, and;
- vii) a control system to control the relative orientation of the first and second links.
- 2. The device of claim 1, at least one of said set of second rotational shafts further comprising an exposed end.
- 3. The device of claim 2, such that at least one member of the first set of leverage points is located coaxially on an exposed end of a member of the set of second rotational shafts.
- 4. The device of claim 1, at least one of said set of first rotational shafts further comprising an exposed end.
- 5. The device of claim 4, such that at least one member of the second set of leverage points is located coaxially on an exposed end of a member of the set of first rotational shafts.
- 6. The device of claim 1, wherein at least one member of the set of first leverage points is located on the yoke of the two-axis Cardan-type joint.
- 7. The device of claim 1, wherein at least one member of the set of second leverage points is located on the yoke of the two-axis Cardan-type joint.
- 8. The device of claim 1, said first and second joints allowing rotational motion only about an axis parallel to the first rotational axis.
- 9. The device of claim 1, said first and second joints allowing rotational motion about axes parallel to the first and second rotational axes.
- 10. The device of claim 1, said third and fourth joints allowing rotational motion only about an axis parallel to the second rotational axis.
- 11. The device of claim 1, said third and fourth joints allowing rotational motion about axes parallel to the first and second rotational axes.
- 12. The device of claim 1, wherein the power source is hydraulic.
- 13. The device of claim 1, wherein the power source is electrical.
- 14. The device of claim 1, said control system comprising rotational encoders.
- 15. The device of claim 1, said control system comprising jet pipe servovalves.
- 16. The device of claim 1, said control system comprising, for each axis of motion, a force feedback loop comprising a servovalve driven by a servo amplifier with an output current proportional to the product of the difference of the desired angle between the first and second links and the actual angle between the first and second links and the effective force being exerted by the appropriate linear actuators.
- 17. The device of claim 16, said control system further comprising a computing system to implement said force feedback loop.
Government Interests
This invention was made with Government support under Contract DE-AC0494DP85000 awarded by the U.S. Department of Energy. The Government has certain rights in the invention.
US Referenced Citations (9)