System for mitigating radiation effects on componentry in space

• US 20050162794A1
• Filed: 10/21/2004
• Published: 07/28/2005
• Est. Priority Date: 10/30/2003
• Status: Abandoned Application

• Current Assignee: Charles F. Green Jr, Craig P. Allen, David S. Donnelly, John P. Lintz
• Original Assignee: Charles F. Green Jr, Craig P. Allen, David S. Donnelly, John P. Lintz
• Inventors: Lintz, John P., Green, Charles F. Jr., Donnelly, David S., Allen, Craig P.
• Application Number:
  US10/969,048
• Publication Number:
  US 20050162794A1
• Time in Patent Office: Days
• US Class Current: 361/93.100
• CPC Class Codes: G01S 19/23 Testing, monitoring, correcting or calibrating of receiver elements

Abstract

A method for mitigating harmful radiation effects on at least one electrical component are disclosed. In a first preferred embodiment, power drawn by the electrical component, such as a GPS receiver, is monitored and compensated by an offset for expected variations due to temperature. When current drawn by the GPS receiver is higher than expected during operation at a given temperature, power to the electrical component is interrupted. Alternatively, or in addition thereto, a second preferred embodiment includes monitoring communications from the GPS receiver. When communications cease or fall below an acceptable level for a predetermined period of time, power to the electrical component is interrupted.

Claims

1. A method for mitigating harmful radiation effects on at least one electrical component, comprising:

supplying interruptible power to the at least one electrical component;

monitoring a first value representative of power drawn by the at least one electrical component;

adjusting, according to an operating temperature, the first value by an offset value and generating an adjusted power;

comparing the adjusted value with a threshold value to determine an overcurrent condition;

interrupting power to the at least one electrical component when an overcurrent condition exists; and

resupplying power to the electrical component after a predetermined period of time so that the electrical component resumes drawing current at a normal level.

2. The method of claim 1, further comprising:

monitoring communications sent from the electrical component;

interrupting power to the electrical component when the communications cease; and

resupplying power after a predetermined period of time has elapsed to the electrical component so that the electrical component resumes sending communications.

3. The method of claim 1, wherein the electrical component comprises a GPS receiver.

4. The method of claim 1, wherein the electrical component is mounted on an object in outer space.

5. The method of claim 1, wherein a power strobe is used to resupply power.

6. The method of claim 1, wherein a sense resistor and an operational amplifier monitor the first value, a temperature sensor provides the offset value, and a comparator compares the adjusted value with a threshold value.

7. A method for mitigating harmful radiation effects on at least one electrical component, comprising:

supplying interruptible power to the at least one electrical component;

monitoring communications sent from the electrical component;

interrupting power to the electrical component when the communications cease; and

resupplying power after a predetermined period of time has elapsed to the electrical component so that the electrical component resumes sending communications.

8. The method of claim 7, further comprising:

monitoring a first value representative of power drawn by the at least one electrical component;

adjusting, according to an operating temperature, the first value by an offset value and generating an adjusted power;

comparing the adjusted value with a threshold value to determine an overcurrent condition;

interrupting power to the at least one electrical component when an overcurrent condition exists; and

resupplying power to the electrical component after a predetermined period of time so that the electrical component resumes drawing current at a normal level.

9. The method of claim 7, wherein the electrical component comprises a GPS receiver.

10. The method of claim 7, wherein the electrical component is mounted on an object in outer space.

11. The method of claim 7, wherein a power strobe is used to resupply power.

12. The method of claim 8, wherein a sense resistor and an operational amplifier monitor the first value, a temperature sensor provides the offset value, and a comparator compares the adjusted value with a threshold value.

13. A method for mitigating harmful radiation effects on at least one electrical component, comprising:

supplying interruptible power to the at least one electrical component;

monitoring a first value representative of power drawn by the at least one electrical component;

adjusting, according to an operating temperature, the first value by an offset value;

comparing the adjusted value with a threshold value to determine an overcurrent condition;

monitoring communications sent from the electrical component;

interrupting power to the at least one electrical component when an overcurrent condition exists or when communications cease; and

resupplying power to the electrical component after a predetermined period of time.

14. A system for mitigating harmful radiation effects on at least one electrical component, comprising:

the electrical component;

a power module for supplying interruptible power to the at least one electrical component; and

an overcurrent detector for monitoring a first value representative of power drawn by the at least one electrical component, adjusting, according to an operating temperature, the first value by an offset value to generate an adjusted value, and comparing the adjusted value with a threshold value to determine an overcurrent condition,

wherein the power supply interrupts power to the at least one electrical component when an overcurrent condition exists and resupplies power to the electrical component after a predetermined period of time sufficient to remove the overcurrent condition.

15. The system of claim 14, further comprising:

a communications detector for monitoring communications sent from the electrical component,

wherein the power supply interrupts power to the electrical component when the communications cease, and resupplies power to the electrical component after a predetermined period of time has elapsed so that the electrical component resumes sending communications.

16. The system of claim 14, wherein the electrical component comprises a GPS receiver.

17. The system of claim 14, wherein the electrical component is mounted on an object in outer space.

18. The system of claim 14, further comprising a power strobe to resupply the power.