Movement detection of hanging loads
Embodiments described herein provide for detecting an angle of a cable attached to a rotorcraft for transporting a hanging payload using a pair of linear displacement sensors that are coupled to both the rotorcraft and the cable. One embodiment is a cable angle detector mounted to an underside of a rotorcraft. A cable has one end coupled to the rotorcraft and another end coupled to a payload. A pair of linear displacement sensors has one end coupled to the underside of the rotorcraft and another end coupled to the cable. The detector measures the displacement of the sensors and calculates an angle of the cable relative to the rotorcraft based on the measurements.
1. An apparatus comprising:
a cable angle detector configured to mount to an underside of a rotorcraft, wherein a cable has a first end coupled to the rotorcraft and a second end coupled to a payload, the cable angle detector including:
a first linear displacement sensor having a first end coupled to the underside of the rotorcraft and a second end coupled to the cable;
a second linear displacement sensor having a first end coupled to the underside of the rotorcraft and a second end coupled to the cable; and
a controller configured to measure a first displacement of the first sensor, to measure a second displacement of the second sensor, and to calculate an angle of the cable relative to the rotorcraft based on the first displacement and the second displacement.
2. The apparatus of claim 1 wherein:
the first end of the first sensor is coupled to the underside of the rotorcraft along a first axis; and
the first end of the second sensor is coupled to the underside of the rotorcraft along a second axis that is perpendicular to the first axis.
3. The apparatus of claim 1 wherein:
the second end of the first sensor and the second end of the second sensor are coupled to the cable at a common location.
4. The apparatus of claim 1 further comprising:
an adapter plate mounted to the rotorcraft;
wherein the first end of the first sensor and the first end of the second sensor are coupled to the adapter plate.
5. The apparatus of claim 1 wherein:
the controller is configured to provide the angle of the cable to a flight system of the rotorcraft for adjusting an orientation of the rotorcraft in flight.
6. The apparatus of claim 1 wherein:
the controller is configured to calculate a position of the payload relative to the rotorcraft based on the angle of the cable.
7. The apparatus of claim 1 wherein:
the first sensor and the second sensor comprise at least one of a linear potentiometer and a string potentiometer.
8. The apparatus of claim 1 wherein:
the rotorcraft comprises an Unmanned Air Vehicle (UAV).
9. A method of monitoring a cable having a first end coupled to a rotorcraft and a second end coupled to a payload, the method comprising:
measuring a first displacement of a first linear displacement sensor having a first end coupled to an underside of the rotorcraft and a second end coupled to the cable;
measuring a second displacement of a second linear displacement sensor having a first end coupled to the underside of the rotorcraft and a second end coupled to the cable; and
calculating an angle of the cable relative to the rotorcraft based on the first displacement and the second displacement.
10. The method of claim 9 wherein:
the first end of the first sensor is coupled to the underside of the rotorcraft along a first axis;
the first end of the second sensor is coupled to the underside of the rotorcraft along a second axis that is perpendicular to the first axis; and
calculating the angle further comprises:
calculating the angle based on an orientation of the first sensor along the first axis and an orientation of the second sensor along the second axis.
11. The method of claim 9 wherein:
the second end of the first sensor and the second end of the second sensor are coupled to the cable at a common location.
12. The method of claim 9 further comprising:
providing the angle of the cable to a flight system of the rotorcraft for adjusting an orientation of the rotorcraft in flight.
13. The method of claim 9 further comprising:
calculating a position of the payload relative to the rotorcraft based on the angle of the cable.
14. An apparatus comprising:
a cable angle detector configured to mount to an underside of a rotorcraft, wherein a cable has a first end coupled to the rotorcraft that defines an origin for a first axis and a second axis that is perpendicular to the first axis, wherein the cable has and a second end coupled to a payload, the cable angle detector including:
a first linear displacement sensor having a first end coupled to the underside of the rotorcraft along the first axis at a first-offset from the origin, wherein the first linear displacement sensor has a second end coupled to the cable;
a second linear displacement sensor having a first end coupled to the underside of the rotorcraft along the second axis at a second-offset from the origin, wherein the second linear displacement sensor has a second end coupled to the cable; and
a controller configured to measure a first displacement of the first sensor, to measure a second displacement of the second sensor, and to calculate an angle of the cable relative to the rotorcraft based on the first displacement, the first-offset, the second displacement, and the second-offset.
15. The apparatus of claim 14 wherein:
the second end of the first sensor and the second end of the second sensor are coupled to the cable at a common location.
16. The apparatus of claim 14 further comprising:
an adapter plate mounted to the rotorcraft;
wherein the first end of the first sensor and the first end of the second sensor are coupled to the adapter plate.
17. The apparatus of claim 14 wherein:
the controller is configured to provide the angle of the cable to a flight system of the rotorcraft for adjusting an orientation of the rotorcraft in flight.
18. The apparatus of claim 14 wherein:
the controller is configured to calculate a position of the payload relative to the rotorcraft based on the angle of the cable.
19. The apparatus of claim 14 wherein:
the first sensor and the second sensor comprise at least one of a linear potentiometer and a string potentiometer.
20. The apparatus of claim 14 wherein:
the rotorcraft comprises an Unmanned Air Vehicle (UAV).