Telemetry for testing switch configuration in ion propulsion system

• US 9,086,060 B1
• Filed: 10/31/2012
• Issued: 07/21/2015
• Est. Priority Date: 10/31/2012
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Stickelmaier, John F., Nguyen, Philip D.
• Primary Examiner(s): Wongwian, Phutthiwat
• Assistant Examiner(s): Breazeal, William
• Application Number:
  US13/664,635
• Time in Patent Office: 993 Days
• Field of Search: 307/18, 307/38, 307/113, 307/125, 307/130
• US Class Current: 1/1
• CPC Class Codes: B64G 1/405 Ion or plasma engines per se F03H1/00
• CPC Class Codes: B64G 1/428 Power distribution and management
• CPC Class Codes: F03H 1/0018 Arrangements or adaptations of power supply systems for cosmonautic vehicles B64G1/42
• CPC Class Codes: G01R 31/3278 of relays, solenoids or reed switches measuring contact resistance G01R27/205; high voltage magnetic switches G01R31/3271, G01R31/333; testing electric windings G01R31/72; monitoring of fail safe circuits H01H47/002
• CPC Class Codes: H01R 29/00 Coupling parts for selective co-operation with a counterpart in different ways to establish different circuits, e.g. for voltage selection, for series-parallel selection, programmable connectors

Abstract

A relay telemetry system enables an ion propulsion system to self-test the critical relay configuration prior to supplying high-voltage power to any thruster. This test detects whether any critical relay has failed to switch properly or is in the wrong configuration. In the test mode, an onboard computer initiates the application of a low-voltage test voltage (nominally 15 V) to the high-voltage circuits (when the high voltage is off) by a stimulus circuit. Sensing circuits detect the inputs and outputs of the system connections in response to this stimulus. If the test voltage appears on an input or output where it is not expected, then a relay fault has occurred and will be detectable in telemetry sent back to the onboard computer.

Claims

1. An ion propulsion system comprising first and second power controllers making available a high-voltage power, first and second ion thrusters and a multiplicity of high-voltage relays, said multiplicity of high-voltage relays having first and second switch states, said first and second power controllers being connected to provide high-voltage power to said first and second thrusters respectively when said multiplicity of high-voltage relays are in said first switch state, said first and second power controllers being connected to provide high-voltage power to said second and first thrusters respectively when said multiplicity of high-voltage relays are in said second switch state, said system further comprising a low-voltage power supply making available a low-voltage power and low-voltage self-test circuitry which is capable of selectively providing said low-voltage power to said high-voltage relays of said multiplicity and detecting voltages in respective conductors of said high-voltage relays when said low-voltage power is provided.

2. The ion propulsion system as recited in claim 1, further comprising a computer system which is connected and programmed to perform the following operations:

initiating the selective providing of low-voltage power to said high-voltage relays by said low-voltage self-test circuitry; and

processing voltages detected by said low-voltage self-test circuitry when said low-voltage power is provided to said high-voltage relays.

3. The ion propulsion system as recited in claim 1, wherein said low-voltage self-test circuitry comprises:

a pulse generator;

a stimulus circuit connected to receive pulses generated by said pulse generator;

a first low-voltage switch connected to said low-voltage power supply and controlled by a pulse from said stimulus circuit, wherein a first high-voltage relay of said multiplicity of high-voltage relays receives a low-voltage pulse from said low-voltage power supply when said first low-voltage switch is turned on by said pulse from said stimulus circuit;

a first sensing circuit for detecting a first voltage in a conductor of said first high-voltage relay when said low-voltage pulse is received by said first high-voltage relay; and

a telemetry output circuit connected to said first sensing circuit.

4. The ion propulsion system as recited in claim 3, further comprising a second low-voltage switch, wherein said stimulus circuit comprises a multiplexer having an input terminal connected to said pulse generator and first and second output terminals respectively connected to said first and second low-voltage switches.

5. The ion propulsion system as recited in claim 3, further comprising a second sensing circuit, wherein said telemetry output circuit comprises a multiplexer having an output terminal and first and second input terminals respectively connected to said first and second sensing circuits.

6. The ion propulsion system as recited in claim 3, wherein said first sensing circuit outputs an encoded analog signal indicative of a state of said first high-voltage relay when said low-voltage pulse is received by said first high-voltage relay.

7. The ion propulsion system as recited in claim 3, further comprising high-voltage resistors which protect the stimulus and sensing circuits.

8. The ion propulsion system as recited in claim 3, wherein a second high-voltage relay of said multiplicity of high-voltage relays also receives said low-voltage pulse from said low-voltage power supply when said first low-voltage switch is turned on by said pulse from said stimulus circuit, further comprising a second sensing circuit for detecting a second voltage in a conductor of said second high-voltage relay when said low-voltage pulse is received by said second high-voltage relay.

9. An electronic system configured to deliver high-voltage power to either of first and second electronic devices of an ion propulsion system, comprising:

a high-voltage power supply making available said high-voltage power;

a multiplicity of high-voltage switching circuits, said multiplicity of high-voltage switching circuits having first and second switch states, wherein said multiplicity of high-voltage switching circuits in said first switch state provides said high-voltage power to said first electronic device and electrically isolates said second electronic device from said high-voltage power supply, and wherein said multiplicity of high-voltage switching circuits in said second switch state provides said high-voltage power to said second electronic device and electrically isolates said first electronic device from said high-voltage power supply;

a low-voltage power supply providing low-voltage power; and

low-voltage self-test circuitry which is capable of selectively providing said low-voltage power to said high-voltage switching circuits and to detect voltages in respective first conductors of said high-voltage switching circuits arising from the application of said low-voltage power to said high-voltage switching circuits.

10. The electronic system as recited in claim 9, further comprising a computer system which is connected and programmed to perform the following operations:

initiating the selective providing of low-voltage power to said high-voltage switching circuits by said low-voltage self-test circuitry; and

processing the respective voltages detected by said low-voltage self-test circuitry when said low-voltage power is provided to said high-voltage switching circuits.

11. The electronic system as recited in claim 9, wherein said high-voltage switching circuits comprise relays.

12. The electronic system as recited in claim 9, wherein said low-voltage self-test circuitry comprises:

a pulse generator;

a stimulus circuit connected to receive pulses generated by said pulse generator;

a first low-voltage switch connected to said low-voltage power supply and controlled by a pulse from said stimulus circuit, wherein a first high-voltage switching circuit of said multiplicity of high-voltage switching circuits receives a low-voltage pulse from said low-voltage power supply when said first low-voltage switch is turned on by said pulse from said stimulus circuit;

a first sensing circuit for detecting a voltage in a conductor of said first high-voltage switching circuit when said low-voltage pulse is received by said first high-voltage switching circuit; and

a telemetry output circuit connected to said first sensing circuit.

13. The electronic system as recited in claim 12, further comprising a second low-voltage switch and a second sensing circuit, wherein said stimulus circuit comprises a first multiplexer having an input terminal connected to said pulse generator and first and second output terminals respectively connected to said first and second low-voltage switches;

and said telemetry output circuit comprises a second multiplexer having an output terminal and first and second input terminals respectively connected to said first and second sensing circuits.

14. A self-testing electronic circuit method for detecting the state of each of the high-voltage switching circuits in the electronic system of claim 9, wherein the high-voltage switching circuits further comprise respective second and third conductors, each respective high-voltage switching circuit having at least a respective first state in which the respective first conductor is connected to the respective second conductor and a respective second state in which the respective first conductor is connected to the respective third conductor, the method comprising:

(a) applying a first low voltage to the respective second conductor of one of the respective high-voltage switching circuits; and

(b) sensing a respective first voltage at the respective first conductor of the one of the respective high-voltage switching circuits when the first low voltage is applied to the respective second conductor.

15. The method as recited in claim 14, further comprising:

(c) applying a second low voltage to the respective third conductor of the one of the respective high-voltage switching circuits; and

(d) sensing the respective second voltage at the respective first conductor of the one of the respective high-voltage switching circuits when the second low voltage is applied to the respective third conductor.

16. The method as recited in claim 15, further comprising:

(e) determining whether or not each of the sensed respective first and second voltages equals zero; and

(f) generating an error signal in response to a determination that each of the sensed respective first and second voltage equals zero.

17. A method for self-testing by an electronic system of claim 9, comprising:

applying a low-voltage test voltage in sequence to other respective conductors of said multiplicity of high-voltage switching circuits; and

sensing the respective voltages which occur at the respective first conductors of said multiplicity of high-voltage switching circuits when the low-voltage test voltages are applied.

18. The method as recited in claim 17, wherein the electronic system is onboard an orbiting spacecraft.

19. The method as recited in claim 18, further comprising transmitting encoded data from the spacecraft to ground, said data being encoded to indicate the sensed voltages.

20. The method as recited in claim 17, further comprising:

determining whether or not the respective voltages as sensed indicate an error condition; and

taking action to correct the error condition prior to delivering high-voltage power to said high-voltage switching circuits.

21. The method as recited in claim 20, wherein each high-voltage switching circuit comprises a relay and said error condition is an improper relay configuration.