Systems and methods for tracker-level protection
A solar tracking system includes a solar array, a support structure configured to support the solar array, a driveshaft coupled to the support structure, a base configured to rotatably support the driveshaft, and an articulation system coupled to the driveshaft and configured to articulate the driveshaft relative to the base. The articulation system includes a gearbox coupled to the driveshaft. The solar tracking system also includes a motor mechanically operably coupled to the gearbox to cause the driveshaft to rotate, and a controller that determines a fault caused by the winding up of the driveshaft, and, in response to determining the fault, shorting the windings of the motor and/or providing power, which is generated by the motor when the unwinding driveshaft drives the rotation of the motor, to a load, such as an energy storage device, a resistive load, and/or a heating element.
1 . A method of articulating a solar tracking system, comprising:
determining a position of the sun relative to a solar array disposed on a driveshaft, the driveshaft rotatably supported by a plurality of bases;
actuating a motor mechanically coupled to the driveshaft based on the determined position of the sun relative to the solar array;
determining a fault caused by a winding up of the driveshaft; and
in response to determining the fault, controlling power circuitry to provide power generated in the motor by an unwinding of the driveshaft to a load.
2 . The method of articulating a solar tracking system according to claim 1 , wherein determining the fault includes detecting the winding up of the driveshaft by a torsion sensor disposed on or in the driveshaft.
3 . The method of articulating a solar tracking system according to claim 1 , further comprising changing a length of a plurality of actuators associated with the plurality of bases to rotate the solar array relative to the plurality of bases, wherein rotation of the solar array corrects an orientation of the solar array relative to the sun.
4 . The method of articulating a solar tracking system according to claim 3 , wherein changing the length of the plurality of actuators includes causing a motor mechanically coupled to a gearbox associated with the plurality of actuators to rotate, wherein rotation of the motor causes the gearbox to change the length of the plurality of actuators.
5 . The method of articulating a solar tracking system according to claim 3 , wherein changing the length of the plurality of actuators includes causing a motor coupled to a plurality of driveshafts to cause a plurality of gearboxes associated with a respective actuator of the plurality of actuators to rotate, wherein rotation of the motor causes the plurality of driveshafts to rotate, which in turn, causes the plurality of gearboxes to change the length of the plurality of actuators, further comprising:
determining a fault caused by a winding up of one of the plurality of driveshafts; and
in response to determining the fault, controlling power circuitry to provide power generated in the motor by an unwinding of the one of the plurality of driveshafts to a load.
6 . The method of articulating a solar tracking system according to claim 3 , wherein changing the length of the plurality of actuators includes causing a plurality of motors coupled to a respective plurality of gearboxes associated with the plurality of actuators to rotate, wherein rotation of the plurality of motors causes each respective gearbox to change the length of each respective actuator of the plurality of actuators.
7 . The method of articulating a solar tracking system according to claim 1 , wherein the load is a battery or a heating element.