Satellite including crossover power processing units for electric thrusters
A spacecraft propulsion system including a first thruster system including a first power processing unit connected to a first thruster string via a crossover switching unit and connected to a second thruster string via the crossover switching unit. A second thruster system including a second power processing unit connected to the second thruster string via the crossover switching unit and to the first thruster string via the crossover switching unit. A controller is connected to each of the first power processing unit, the second power processing unit, and the crossover switching unit.
1. A spacecraft propulsion system comprising:
a first thruster system including a first power processing unit connected to a first thruster string via a crossover switching unit and connected to a second thruster string via the crossover switching unit;
a second thruster system including a second power processing unit connected to the second thruster string via the crossover switching unit and to the first thruster string via the crossover switching unit, wherein the second power processing unit is separate from the first power processing unit, and the first power processing unit and the second power processing unit are included in respective ones of the first thruster system and the second thruster system; and
a controller connected to each of the first power processing unit, the second power processing unit, and the crossover switching unit;
wherein the crossover switching unit includes a first plurality of switches and a second plurality of switches; and
wherein each switch in the first plurality of switches and the second plurality of switches is a latching relay with input terminals respectively connected to the first power processing unit and the second power processing unit and configured to switch a connection to the first thruster string or the second thruster string between the first power processing unit and the second power processing unit.
2. The spacecraft propulsion system of claim 1 , wherein the first thruster string and the second thruster string each include at least two thrusters.
3. The spacecraft propulsion system of claim 2 , wherein the at least two thrusters in each of the first thruster string and the second thruster string are electric thrusters.
4. The spacecraft propulsion system of claim 3 , wherein the at least two thrusters in each of the first thruster string and the second thruster string are hall effect electric thrusters.
5. The spacecraft propulsion system of claim 1 , wherein the first plurality of switches in the crossover switching unit and the second plurality of switches in the crossover switching unit are approximately identical.
6. The spacecraft propulsion system of claim 1 , wherein the crossover switching unit includes seven latching relays per thruster in each respective corresponding thruster string.
7. The spacecraft propulsion system of claim 1 , wherein the controller includes a control module configured to demultiplex an output of one of the first power processing unit and the second power processing unit using the crossover switching unit, such that the first power processing unit provides output signals to the first thruster string and the second thruster string.
8. A method for providing crossover redundancy in a spacecraft propulsion system comprising:
connecting a first power processing unit to a first thruster string using a crossover switching unit and to a second thruster string using the crossover switching unit;
connecting a second power processing unit to the first thruster string using the crossover switching unit and to the second thruster string using the crossover switching unit, wherein the second power processing unit is separate from the first power processing unit and the first power processing unit and the second power processing unit are included in respective ones of the first thruster system and the second thruster system;
connecting a controller to each of the first power processing unit, the second power processing unit, and the crossover switching unit; and
controlling the crossover switching unit with the controller such that the first power processing unit signals are passed through the crossover switching unit to the first thruster string and the second power processing unit signals are passed through the crossover switching unit to the second thruster string;
wherein the controlling the crossover switching unit with the controller includes commanding a state of each switch in a first plurality of switches within the crossover switching unit and commanding a state of each switch in a second plurality of switches within the crossover switching unit using the controller; and
wherein each switch in the first plurality of switches and the second plurality of switches is a latching relay with input terminals respectively connected to the first power processing unit and the second power processing unit and configured to switch a connection to the first thruster string or the second thruster string between the first power processing unit and the second power processing unit.
9. The method of claim 8 , further comprising: controlling the crossover switching unit with the controller such that the crossover switching unit demultiplexes signals from the first power processing unit to the first thruster string and the second thruster string in response to a fault in the second power processing unit.
10. The method of claim 8 , wherein controlling the crossover switching unit with the controller comprises connecting each power processing unit of the first power processing unit and the second power processing unit to the corresponding thruster string as a single unit.
11. The method of claim 8 , wherein controlling the crossover switching unit with the controller comprises connecting each power processing unit of the first power processing unit and the second power processing unit to each thruster of the first thruster string and the second thruster string independently.