Robotic landing gear for rotorcraft
The present invention relates to robotic landing gear for a rotorcraft that is designed to allow for landing on sloped and irregular surfaces. The robotic landing gear consists of articulated legs with contact sensors. Once the contact sensor touches a landing surface, the articulated leg in which contact is detected retracts to maintain a certain amount of contact pressure with the surface. Each articulated leg does this independently until contact is detected on the sensors of all of the robotic legs, at which point the legs lock in position and the rotorcraft can safely land.
1. A robotic landing gear apparatus for a rotorcraft for landing the rotorcraft on a surface comprising:
a plurality of independent articulated robotic legs attached to the rotorcraft wherein each of the articulated robotic legs further comprises:
an upper leg segment further comprising an upper leg segment top and an upper leg segment bottom, wherein the upper leg segment top is movably attached to the rotorcraft to form a hip joint,
a hip joint actuator, for moving the upper leg segment in relation to the rotorcraft,
a means for locking the hip joint, and
a lower leg segment, wherein the lower leg segment further comprises a lower leg segment moveably attached to the upper leg segment bottom to form a knee joint,
a knee joint actuator, for moving the lower leg segment and upper leg segment about the knee joint,
a means for locking the knee joint, and
a knee joint sensor, wherein the knee joint sensor senses the actuation of the knee joint actuator and motion of the lower leg segment and upper leg segment about the knee joint, and
a foot attached to the lower leg segment bottom, wherein the foot further comprises a contact sensor.
2. The robotic landing gear apparatus of claim 1 wherein the hip joint actuator is an electric motor connected to the hip joint by means of a hip joint gearbox and the knee joint actuator is an electric motor attached to the knee joint by means of a knee joint gearbox.
3. The robotic landing gear apparatus of claim 1 wherein the means for locking the hip joint is a hip joint power-off brake and the means for locking the knee joint is a knee joint power-off brake.
4. The robotic landing gear apparatus of claim 1 wherein the contact sensor comprises a pressure-sensitive film wherein the pressure-sensitive film is located between at leas to layers of conductive film.
5. The robotic landing gear of claim 1 wherein the knee joint sensor is an absolute encoder.
6. The robotic landing gear of claim 1 wherein when the contact sensor senses contact with the surface, the hip joint actuator and the knee joint actuator actuate to retract the upper leg segment and lower leg segment to maintain contact with the surface.
7. The robotic landing gear of claim 1 wherein the hip joint is a hinge joint.
8. The robotic landing gear of claim 1 wherein the hip joint is a ball and socket joint.
9. A robotic landing gear apparatus for a rotorcraft for landing the rotorcraft on a surface comprising:
at last three independent articulated robotic legs attached to the rotorcraft wherein each of the at least three articulated robotic legs further comprises:
an upper leg segment further comprising an upper leg segment top and an upper leg segment bottom, wherein the upper leg segment is movably attached to the rotor craft to form a hip joint,
a hip joint actuator for moving the upper leg segment in relation to the rotorcraft,
a means for locking the hip joint,
a lower leg segment further comprising a lower leg segment top and a lower leg segment bottom, wherein the lower leg segment is movably attached to the upper leg segment to form a knee joint,
a knee joint actuator for moving the lower leg segment in relation to the upper leg segment,
a means for locking the knee joint,
a foot attached to the lower leg segment bottom, wherein the foot further comprises a contact sensor, wherein when the contact sensor senses contact with the surface, the hip joint actuator and the knee joint actuator actuate to retract the upper leg segment and lower leg segment to maintain contact with the surface, and
wherein the plurality of articulated robotic legs are controlled independent of each other.
10. The robotic landing gear apparatus of claim 9 wherein the hip joint actuator is an electric motor attached to the hip joint by means of a hip joint gearbox and the knee joint actuator is an electric motor attached to the knee joint by means of a knee joint gearbox.
11. The robotic landing gear apparatus of claim 9 wherein the means for locking the hip joint is a hip joint power-off brake and the means for locking the knee joint is a knee joint power-off brake.
12. The robotic landing gear apparatus of claim 9 wherein the contact sensor comprises a pressure-sensitive film wherein the pressure-sensitive film is located between at least two layers of conductive film.
13. The robotic landing gear of claim 9 wherein the knee joint sensor is an absolute encoder.
14. The robotic landing gear of claim 9 wherein the hip joint is a hinge joint.
15. The robotic landing gear of claim 9 wherein the hip joint is a ball and socket joint.
16. The robotic landing gear of claim 9 wherein the contact sensors of each independently articulated leg maintain contact pressure with the surface until each of the contact sensors of each of the independently articulated leg senses the surface.