Satellite charge monitor

• US 6,844,714 B2
• Filed: 02/21/2003
• Issued: 01/18/2005
• Est. Priority Date: 02/21/2003
• Status: Expired due to Fees

• Current Assignee: Gerald R. Dubois, Keith G. Balmain, Peter C. Kremer
• Original Assignee: Gerald R. Dubois, Keith G. Balmain, Peter C. Kremer
• Inventors: Dubois, Gerald R., Balmain, Keith G., Kremer, Peter C.
• Primary Examiner(s): Patidar, Jay
• Assistant Examiner(s): NGUYEN, HOAI AN D
• Application Number:
  US10/369,521
• Publication Number:
  US 20040166814A1
• Time in Patent Office: 697 Days
• Field of Search: 324/72, 324/71.3, 324/71.4, 324/76.11, 324/678, 324/72.5, 324/96, 324/446, 324/447, 324/450, 244/158.R, 244/173, 244/1.A, 136/244, 136/292, 320/101, 320/136, 342/352, 348/117, 701/13, D12/319, D12/320, 250/326, 250/397, 250/305, 250/336.1, 250/363.01, 315/111.81, 361/218
• US Class Current: 324/72
• CPC Class Codes: B64G 1/546 shielding electronic equipment

Abstract

The present invention provides a charge monitor for satellites for monitoring build up of electric charge due to charge particle fluxes impinging on the satellite. In one aspect of the invention the charge monitor includes an electrically conducting housing including at least two compartments with each compartment including a dielectric slab contained therein. An electrically conducting electrode is embedded in each dielectric slab a pre-selected distance below a top surface of the dielectric slab, the housing being mountable on a satellite with the top surface of the dielectric slab facing outwardly into space away from the satellite whereby charged particles emitted from sources external to the satellite penetrate the dielectric slab resulting in charge accumulation in each electrically conducting electrode, each electrically conducting electrode being electrically isolated from all other electrically conducting electrodes in the electrically conducting housing. The monitor includes an electrical voltage detector for sensing the floating DC voltage developed on the electrically conducting electrode in each dielectric slab, due to the charge accumulation, and converting the DC voltage into an AC voltage representative of a charge buildup on each electrically conducting electrode.

Claims

1. A charge monitor for satellites, comprising:

a) an electrically conducting housing including at least two compartments with said at least two compartments each including a dielectric slab contained therein, each dielectric slab having a selected thickness;

b) an electrically conducting electrode embedded in each dielectric slab a pre-selected distance below a top surface of the dielectric slab, said housing being mountable on a satellite with said top surface of said dielectric slab facing outwardly into space away from said satellite whereby charged particles emitted from sources external to the satellite penetrate said dielectric slab resulting in charge accumulation in each electrically conducting electrode producing a floating DC voltage on said electrically conducting electrode, each electrically conducting electrode being electrically isolated from all other electrically conducting electrodes in said electrically conducting housing; and

c) detection means for sensing of the floating DC voltage developed on the electrically conducting electrode embedded in each dielectric slab, due to the charge accumulation, and converting the floating DC voltage into an AC voltage representative of a charge buildup on each electrically conducting electrode.

2. The charge monitor according to claim 1 wherein said at least two compartments is two or more compartments which are arranged side-by-side for measuring charge build-up over a pre-selected surface area, and wherein the electrically conducting electrodes are embedded at different depths for measuring charge build-up at the different depths in the dielectric slabs.

3. The charge monitor according to claim 2 wherein the dielectric slab in each compartment contains a dielectric slab made of a dielectric material different from the dielectric slabs in the other compartments with each dielectric material corresponding to a dielectric component of a satellite.

4. The charge monitor according to claim 3 wherein said dielectric material from which said dielectric slabs are produced is selected from the group consisting of Mylar, Kapton, Rexolite, Kevlar, Teflon, acrylic, ceramic, fiberglass, and composites thereof.

5. The charge monitor according to claim 1 wherein said detection means includes a number of electrically conducting sensing posts equal to a number of said electrically conductive electrodes, said electrically conducting sensing posts being arranged in a circle, including a cylindrical electrically conductive housing having a pre-selected number of slots in a side wall thereof being mounted with said electrically conducting sensing posts being located within said cylindrical electrically conductive housing, said cylindrical electrically conductive housing being connected to a motor for rotation about a cylindrical axis of said cylindrical electrically conductive housing, and wherein said detection means includes a number of electrically conducting charging posts equal to the number of said electrically conductive electrodes, each of said electrically conducting electrodes being connected to an associated electrically conducting charging post, the electrically conducting charging posts being arranged in a circle on the outside of said cylindrical electrically conductive housing and concentric with the circle of the electrically conductive sensing posts so that each electrically conductive sensing post is in opposing relationship to an associated electrically conducting charging post, said detection means including a voltage measuring means connected to each electrically conducting sensing post, wherein as said cylindrical electrically conductive housing rotates, each time a slot is rotated into a position between an electrically conducting sensing post and its associated electrically conducting charging post, an electric field is established therebetween and the voltage induced on said electrically conducting sensing post from the floating DC voltage on the electrically conducting charging post is measured, and wherein rotating said slot into, and out of, the position between said electrically conducting sensing post and its associated electrically conducting charging post periodically turns on, and off, the electric field that passes therebetween thereby converting the floating DC voltage on the electrically conducting electrode embedded in the dielectric slab into an alternating voltage on the electrically conducting sensing post.

6. The charge monitor according to claim 5 wherein said voltage measuring means includes an amplifier means connected to each of said electrically conducting sensing post for providing an amplified voltage signal proportional to the alternating voltage on the electrically conducting sensing post.

7. The charge monitor according to claim 6 wherein each amplifier means includes two operational amplifier stages, a first operational amplifier stage through which the alternating signal from the electrically conducting sensing post is passed to amplify the alternating signal, and a second operational amplifier stage functioning as a synchronous detector, and wherein said cylindrical electrically conductive housing includes a peripheral notched rim, including an optical reader circuit mounted in said electrically conducting housing and including a light source and light detector means, said light source and detection means being positioned so that light from said light source is periodically reflected from said peripheral notched rim and detected by said detection means producing an alternating optical signal, said alternating optical signal being passed through a rectifier means whose output turns on and off an associated operational amplifier in synchronism with one of the slot being rotated into, and out of, the position between the electrically conducting sensing post and its associated electrically conducting charging post.

8. The charge monitor according to claim 7 wherein the direct current (DC) voltage on the electrically conducting charging post produces a unipolar electric field around the electrically conductive charging post which is transformed into said AC voltage which is a bipolar-pulse signal emerging from the electrically conducting sensing post, and wherein each second operational amplifier stage functioning as a synchronous detector is “

on”

only during a unipolar part of the bipolar pulse signal so that a rectified and filtered output voltage of the second operational amplifier stage is configured to have the same sign as the charging potential that is being measured.

9. The charge monitor according to claim 5 wherein said dielectric slabs are spaced sufficiently far enough from each other, said electrically conducting charging posts are spaced sufficiently far enough from each other and said slots are spaced sufficiently far enough from each other in the wall of said cylindrical electrically conductive housing to reduce electrical interference of a measurement of a voltage induced on one of said electrically conducting sensing posts from measurements of voltages on the other electrically conducting sensing posts being simultaneously measured through the other slots.

10. The charge monitor according to claim 5 wherein said at least two compartments is greater than two compartments which are arranged side-by-side for measuring charge build-up over a pre-selected surface area, and wherein the electrically conducting electrodes are embedded at different depths for measuring charge build-up at the different depths in the dielectric slabs.

11. The charge monitor according to claim 10 wherein each compartment contains a dielectric slab made of a dielectric material different from the dielectric slabs in the other compartments with each dielectric material corresponding to a dielectric component of a satellite.

12. The charge monitor according to claim 11 wherein said dielectric material from which said dielectric slabs are produced is selected from the group consisting of Mylar, Kapton, Rexolite, Kevlar, Teflon, acrylic, ceramics, fiberglass, and composites thereof.

13. The charge monitor according to claim 1 wherein said detection means comprises a pre-selected number of transducers equal to the number of said electrically conducting electrodes,

each transducer including a first metallic diaphragm electrically connected to an associated electrically conducting electrode, a second metallic diaphragm spaced from said first metallic diaphragm and substantially parallel thereto on one side of said first metallic diaphragm, a means for vibrating said second metallic diaphragm at a pre-selected frequency, and a third metallic diaphragm located on the other side of said first metallic diaphragm and substantially parallel thereto, said first metallic diaphragm being electrically insulated so that it acquires the floating voltage potential developed on the electrically conducting electrode to which it is attached,

said detection means including an oscillator circuit connected to said vibration means and a synchronous detection circuit electrically connected to said third metallic diaphragm, wherein vibrating said second metallic diaphragm at said pre-selected frequency produces an oscillating capacitance to the first metallic diaphragm which then induces an oscillating charge on said third metallic diaphragm, resulting in an oscillating current at said pre-selected frequency being injected into the synchronous detection circuit which converts said oscillating current into a DC voltage proportional to the floating DC voltage on the electrically conducting electrode.

14. The charge monitor according to claim 13 wherein said at least two dielectric slabs is a plurality of dielectric slabs arranged in a plane, wherein said electrically conducting electrodes embedded in each dielectric slab are elongate wires disposed parallel to the top surface of the slabs in which they are embedded, wherein said elongate wires are embedded at different depths in their respective dielectric slabs to allow monitoring at those depths of the potentials due to charge accumulation.

15. The charge monitor according to claim 13 wherein said detection means includes amplifier means through which said oscillating current passes, said amplifier means being connected to said synchronous detection circuit, said synchronous detection including an amplifier turned on and off at half-cycle intervals as a consequence of a half-wave rectifier means operating on a fraction of the oscillator circuit signal and wherein another fraction of the oscillator circuit signal drives the vibration means, and wherein a half-wave-rectified signal is filtered through a filter means to remove ripple and is then passed to a DC amplifier means the output of which is the DC voltage signal proportional to the floating DC voltage on the electrically conducting electrode.

16. The charge monitor according to claim 15 wherein said vibration means is a piezoelectric crystal bonded to said second metallic diaphragm.

17. The charge monitor according to claim 15 including voltage digitization means for converting said DC voltage signal to a digital signal, and data storage, retrieval and transmission means for storing, retrieving and transmitting said digital signal.

18. The charge monitor according to claim 13 wherein each compartment contains a dielectric slab made of a dielectric material different from the dielectric slabs in the other compartments with each dielectric material corresponding to a dielectric component of a satellite.

19. The charge monitor according to claim 18 wherein said dielectric material from which said dielectric slabs are produced is selected from the group consisting of Mylar, Kapton, Rexolite, Kevlar, Teflon, acrylic, ceramic, fiberglass, and composites thereof.

20. A charge monitor for satellites, comprising:

a sensor array including at least one sensor unit with the sensor array being attachable to a satellite;

said at least one sensor unit including

a) an electrically conducting housing defining a compartment containing a dielectric slab therein, said dielectric slab having a selected thickness, the electrically conductive housing being attachable to a satellite;

b) an electrically conducting electrode embedded in said dielectric slab a pre-selected distance below a top surface of the dielectric slab, said housing being mountable on a satellite with said top surface of said dielectric slab facing outwardly into space away from said satellite whereby charged particles emitted from sources external to the satellite penetrate said dielectric slab resulting in charge accumulation in the electrically conducting electrode to produce a floating DC voltage, and

c) detection means for sensing the floating DC voltage developed on the electrically conducting electrode in said dielectric slab, due to the charge accumulation, and converting the floating DC voltage into an AC voltage representative of a charge buildup on said electrically conducting electrode.

21. The charge monitor according to claim 20 wherein said at least one sensor unit is two or more sensor units pre-positioned with respect to each other.

22. The charge monitor according to claim 20 wherein said detection means includes a synchronous detection circuit, a first metallic diaphragm electrically connected to said electrically conducting electrode so that it acquires the floating DC voltage potential developed on the electrically conducting electrode to which it is attached, an electrically grounded second metallic diaphragm spaced from said first metallic diaphragm and substantially parallel thereto, vibration means for vibrating said second metallic diaphragm at a pre-selected frequency to oscillate a capacitance between said first and second metallic diaphragms, said first metallic diaphragm being capactively coupled to said synchronous detection circuit wherein said oscillating capacitance induces an oscillating charge on said first metallic diaphragm, resulting in an oscillating current at said pre-selected frequency being injected into the synchronous detection circuit, and wherein said synchronous detection circuit converts said oscillating capacitance to a steady state voltage output indicative of the floating DC voltage buildup on the electrically conducting electrode.

23. The charge monitor according to claim 22 wherein said detection means includes an oscillator circuit connected to said vibration means for oscillating said vibration means at said pre-selected frequency, said oscillator circuit being connected to said synchronous detection circuit, and wherein said detection means includes an amplifier means through which said oscillating current passes, said amplifier means being connected to said synchronous detection circuit, said synchronous detection means including an amplifier turned on and off at half-cycle intervals as a consequence of a half-wave rectifier means operating on a fraction of the oscillator circuit signal and wherein another fraction of the oscillator circuit signal drives the vibration means, and wherein a half-wave-rectified signal is filtered through a filter means to remove ripple and is then passed to a DC amplifier means the output of which is the DC voltage signal proportional to the original DC voltage induced in the electrically conducting electrode embedded in the dielectric slab.

24. The charge monitor according to claim 23 wherein said vibration means is a piezoelectric crystal bonded to said second metallic diaphragm.

25. The charge monitor according to claim 23 including a voltage digitization means for converting said DC voltage signal to a digital signal, and data storage, retrieval and transmission means for storing, retrieving and transmitting said digital signal.

26. The charge monitor according to claim 21 wherein each sensor unit contains a dielectric slab made of a dielectric material different from the dielectric slabs in the other compartments with each dielectric material corresponding to a dielectric component of a satellite.

27. The charge monitor according to claim 26 wherein said dielectric material from which said dielectric slabs are produced is selected from the group consisting of Mylar, Kapton, Rexolite, Kevlar, Teflon, acrylic, ceramic, fiberglass, and composites thereof.

28. The charge monitor according to claim 20 wherein said first metallic diaphragm is capactively coupled to said synchronous detection circuit using at least one capacitor having a sufficiently high voltage rating to protect against an expected maximum floating potential of at least about 15 kV.

29. The charge monitor according to claim 28 wherein said at least one capacitor is three capacitors electrically connected in series with an end-to-end voltage rating of about 30 kV.

30. The charge monitor according to claim 21 wherein said at least two sensor units are arranged side-by-side for measuring charge build-up over a pre-selected surface area, and wherein the electrically conducting electrodes are embedded at different depths in their respective dielectric slabs for measuring charge build-up at the different depths in the dielectric slabs.

31. A satellite, comprising:

a) a satellite housing containing a power supply and a satellite payload including communication means for communicating with a satellite control center;

b) a charge monitor including

an electrically conducting housing including at least two compartments with said at least two compartments each including a dielectric slab contained therein, each dielectric slab having a selected thickness, an electrically conducting electrode embedded in each dielectric slab a pre-selected distance below a top surface of the dielectric slab, said housing being mounted on said satellite housing with said top surface of said dielectric slab facing outwardly into space away from said satellite whereby charged particles emitted from sources external to the satellite penetrate said dielectric slab resulting in charge accumulation in each electrically conducting electrode producing a floating DC voltage on each electrically conducting electrode, each electrically conducting electrode being electrically isolated from all other electrically conducting electrodes in said electrically conducting housing; and

detection means for sensing of the floating DC voltage developed on the electrically conducting electrode embedded in each dielectric slab, due to the charge accumulation, and converting the floating DC voltage into an AC voltage representative of a charge buildup on each electrically conducting electrode,

said charge monitor being connected to said communication means for communicating charge build-up data to the satellite control center.

32. The satellite according to claim 31 wherein said at least two compartments is greater than two compartments which are arranged side-by-side for measuring charge build-up over a pre-selected surface area, and wherein the electrically conducting electrodes are embedded at different depths for measuring charge build-up at the different depths in the dielectric slabs.

33. The satellite according to claim 31 wherein said detection means includes a number of electrically conducting sensing posts equal to a number of said electrically conductive electrodes, said electrically conducting sensing posts being arranged in a circle, including a cylindrical electrically conductive housing having a pre-selected number of slots in a side wall thereof being mounted with said electrically conducting sensing posts being located within said cylindrical electrically conductive housing, said cylindrical electrically conductive housing being connected to a motor for rotation about a cylindrical axis of said cylindrical electrically conductive housing, and wherein said detection means includes a number of electrically conducting charging posts equal to the number of said electrically conductive electrodes, each of said electrically conducting electrodes being connected to an associated electrically conducting charging post, the electrically conducting charging posts being arranged in a circle on the outside of said cylindrical electrically conductive housing and concentric with the circle of the electrically conductive sensing posts so that each electrically conductive sensing post is in opposing relationship to an associated electrically conducting charging post, said detection means including a voltage measuring means connected to each electrically conducting sensing post, wherein as said cylindrical electrically conductive housing rotates, each time a slot is rotated into a position between an electrically conducting sensing post and its associated electrically conducting charging post, an electric field is established therebetween and the voltage induced on said electrically conducting sensing post from the floating DC voltage on the electrically conducting charging post is measured, and wherein rotating said slot into, and out of, the position between said electrically conducting sensing post and its associated electrically conducting charging post periodically turns on, and off, the electric field that passes therebetween thereby converting the floating DC voltage on the electrically conducting electrode embedded in the dielectric slab into an alternating voltage on the electrically conducting sensing post.

34. The satellite according to claim 33 wherein said voltage measuring means includes an amplifier means connected to each of said electrically conducting sensing post for providing an amplified voltage signal proportional to the alternating voltage on the electrically conducting sensing post.

35. The satellite according to claim 34 wherein each amplifier means includes two operational amplifier stages, a first operational amplifier stage through which the alternating signal from the electrically conducting sensing post is passed to amplify the alternating signal, and a second operational amplifier stage functioning as a synchronous detector, and wherein said cylindrical electrically conductive housing includes a peripheral notched rim, including an optical reader circuit mounted in said electrically conducting housing and including a light source and light detector means, said light source and detection means being positioned so that light from said light source is periodically reflected from said peripheral notched rim and detected by said detection means producing an alternating optical signal, said alternating optical signal being passed through a rectifier means whose output turns on and off an associated operational amplifier in synchronism with one of the slot being rotated into, and out of, the position between the electrically conducting sensing post and its associated electrically conducting charging post.

36. The satellite according to claim 35 wherein the direct current (DC) voltage on the electrically conducting charging post produces a unipolar electric field around the electrically conducting sensing post which is transformed into said AC voltage which is a bipolar-pulse signal emerging from the electrically conducting sensing post, and wherein each second operational amplifier stage functioning as a synchronous detector is “

on”

only during a unipolar part of the bipolar pulse signal so that a rectified and filtered output voltage of the second operational amplifier stage is configured to have the same sign as the charging potential that is being measured.

37. The satellite according to claim 33 wherein said dielectric slabs are spaced sufficiently far enough from each other, said electrically conducting charging posts are spaced sufficiently far enough from each other and said slots are spaced sufficiently far enough from each other in the side wall of said cylindrical electrically conductive housing to reduce electrical interference of a measurement of a voltage induced on one of said electrically conducting sensing posts from measurements of voltages on the other electrically conducting sensing posts being simultaneously measured through the other slots.

38. The charge monitor according to claim 36 wherein each compartment contains a dielectric slab made of a dielectric material different from the dielectric slabs in the other compartments with each dielectric material corresponding to a dielectric component of a satellite.

39. The satellite according to claim 38 wherein a material from which said dielectric slabs are produced is selected from the group consisting of Mylar, Kapton, Rexolite, Kevlar, Teflon, acrylic, ceramic, fiberglass, and composites thereof.

40. A satellite, comprising:

a satellite housing containing a power supply, satellite payload including communication means for communicating with a satellite control center; and

a charge monitor including

a sensor array including at least one sensor unit with the sensor array being attached to the satellite housing,

said at least one sensor unit including

a) an electrically conducting housing defining a compartment containing a dielectric slab therein, said dielectric slab having a selected thickness, the electrically conductive housing being attachable to a satellite;

b) an electrically conducting electrode embedded in said dielectric slab a pre-selected distance below a top surface of the dielectric slab, said housing being mountable on a satellite with said top surface of said dielectric slab facing outwardly into space away from said satellite whereby charged particles emitted from sources external to the satellite penetrate said dielectric slab resulting in charge accumulation in the electrically conducting electrode to produce a floating DC voltage, and

c) detection means for sensing the floating DC voltage developed on the electrically conducting electrode in said dielectric slab, due to the charge accumulation, and converting the floating DC voltage into an AC voltage representative of a charge buildup on said electrically conducting electrode.

41. The satellite according to claim 40 wherein said at least one sensor unit is two or more sensor units pre-positioned with respect to each other.

42. The satellite according to claim 41 wherein said detection means includes a synchronous detection circuit, a first metallic diaphragm electrically connected to said electrically conducting electrode so that it acquires the floating DC voltage potential developed on the electrically conducting electrode to which it is attached, an electrically grounded second metallic diaphragm spaced from said first metallic diaphragm and substantially parallel thereto, vibration means for vibrating said second metallic diaphragm at a pre-selected frequency to oscillate a capacitance between said first and second metallic diaphragms, said first metallic diaphragm being capactively coupled to said synchronous detection circuit wherein said oscillating capacitance induces an oscillating charge on said first metallic diaphragm, resulting in an oscillating current at said pre-selected frequency being injected into the synchronous detection circuit, and wherein said synchronous detection circuit converts said oscillating capacitance to a steady state voltage output indicative of the floating DC voltage buildup on the electrically conducting electrode.

43. The satellite according to claim 42 wherein said detection means includes an oscillator circuit connected to said vibration means for oscillating said vibration means at said pre-selected frequency, said oscillator circuit being connected to said synchronous detection circuit, and wherein said detection means includes an amplifier means through which said oscillating current passes, said amplifier means being connected to said synchronous detection circuit, said synchronous detection means including an amplifier turned on and off at half-cycle intervals as a consequence of a half-wave rectifier means operating on a fraction of the oscillator circuit signal and wherein another fraction of the oscillator circuit signal drives the vibration means, and wherein a half-wave-rectified signal is filtered through a filter means to remove ripple and is then passed to a DC amplifier means the output of which is the DC voltage signal proportional to the floating DC voltage induced in the electrically conducting electrode embedded in the dielectric slab.

44. The satellite according to claim 43 wherein said vibration means is a piezoelectric crystal bonded to said second metallic diaphragm.

45. The satellite according to claim 43 including a voltage digitization means for converting said DC voltage signal to a digital signal, and data storage, retrieval and transmission means for storing, retrieving and transmitting said digital signal.

46. The satellite according to claim 41 wherein each sensor unit contains a dielectric slab made of a dielectric material different from the dielectric slabs in the other compartments with each dielectric material corresponding to a dielectric component of a satellite.

47. The satellite according to claim 46 wherein said dielectric material from which said dielectric slabs are produced is selected from the group consisting of Mylar, Kapton, Rexolite, Kevlar, Teflon, acrylic, ceramic, fiberglass, and composites thereof.