Systems and methods for nuclear event circumvention in an inertial device

Patent metadata

Field	Value
Publication number	US-2016377645-A1
Application number	US-2785408-A
Country	US
Kind code	A1
Filing date	Feb 7, 2008
Priority date	Feb 7, 2008
Publication date	Dec 29, 2016
Grant date	—

Abstract

Systems and methods with the ability to raise the set point temperature immediately after a temperature increase due to radiation exposure, thereby reducing T-dot (rate of change in temperature) errors when trying to cool the inertial system back to its original set point temperature. An example system includes an inertial instrument, a sensor that senses if an increased temperature event has been experienced by the inertial instrument, and a controller device that will increase the set point temperature of the inertial instrument based on the determined increase in temperature. The controller device will also maintain the inertial instrument at a temperature associated with at least one of the sensed increased temperature event or the increased set point temperature.

First claim

1 - 10 . (canceled)

11 . An inertial system having a set point temperature, the system comprising:
an inertial instrument; a sensor configured to sense if an increased temperature event has been experienced by the inertial instrument; and a controller device configured to increase the set point temperature of the inertial instrument in response to sensing of the increased temperature event sensed by the sensor, wherein the controller device is configured to maintain the inertial instrument at a temperature associated with at least one of the sensed increased temperature event or the increased set point temperature.

12 . The system of claim 11 , wherein the inertial instrument comprises one or more vibrating beam accelerometers, and wherein one of the one or more vibrating beam accelerometers comprises a proof mass, a stable member and at least one hinge configured to flexibly attach the proof mass to the stable member within a housing.

13 . The system of claim 12 , wherein the sensor comprises one or more temperature sensors.

14 . The system of claim 12 , wherein the sensor comprises one or more radiation sensors configured to produce a radiation value.

15 . The system of claim 14 , wherein the temperature associated with at least one of the sensed increased temperature event or the increased set point temperature is based on the radiation value.

16 . The system of claim 15 , wherein the radiation value includes gamma radiation levels.

17 . The system of claim 12 , further comprising:
a device configured to determine acceleration values based on signals produced by the one or more vibrating beam accelerometers and the increased set point temperature.

18 . The system of claim 12 , wherein the controller device comprises a heating device configured to apply heat to at least one of a cavity within the housing or the stable member.

19 . The system of claim 18 , wherein the controller device maintains the inertial instrument at the temperature associated with at least one of the sensed increased temperature event or the increased set point temperature after effects of the increased temperature event are no longer experienced.

20 . The system of claim 11 , wherein the inertial system comprises one or more gyros or other inertial instruments that experience a temperature rate of change effect.

21 . An inertial system having a set point temperature, the system comprising:
means for sensing an acceleration; means for sensing if an increased temperature event has been experienced by an inertial instrument; and means for increasing the set point temperature of the inertial instrument in response to sensing of the increased temperature event sensed by the means for sensing and maintaining the inertial instrument at a temperature associated with at least one of the sensed increased temperature event or the increased set point temperature.

22 . The system of claim 21 , wherein the means for sensing the acceleration comprises one or more vibrating beam accelerometers, and wherein one of the one or more vibrating beam accelerometers comprises a proof mass, a stable member and at least one hinge configured to flexibly attach the proof mass to the stable member within a housing.

23 . The system of claim 22 , wherein the means for sensing the temperature event comprises one or more temperature sensors.

24 . The system of claim 22 , wherein the means for sensing the temperature event comprises one or more radiation sensors configured to produce a radiation value.

25 . The system of claim 24 , wherein the temperature associated with at least one of the sensed increased temperature event or the increased set point temperature is based on the radiation value.

26 . The system of claim 25 , wherein the radiation value includes gamma radiation levels.

27 . The system of claim 22 , further comprising:
means for determining acceleration values based on signals produced by the one or more vibrating beam accelerometers and the increased set point temperature.

28 . The system of claim 22 , wherein the means for increasing the set point temperature comprises a heating device configured to apply heat to at least one of a cavity within the housing or the stable member.

29 . The system of claim 28 , wherein the means for increasing the set point temperature further maintains the inertial instrument at the temperature associated with at least one of the sensed increased temperature event or the increased set point temperature after effects of the increased temperature event are no longer experienced.

30 . A method for operating an inertial system having a set point temperature, the method comprising:
sensing, by a sensor, an increased temperature event experienced by the inertial system; in response to sensing the increased temperature event, increasing the set point temperature of the inertial system; and maintaining the inertial system at a temperature associated with at least one of the sensed increased temperature event or the increased set point temperature.

Assignees

• Meyer Robert
• Honeywell Int Inc

Inventors

• Meyer Robert

Classifications

• G01P15/02

  by making use of inertia forces {using solid seismic masses}(G01P15/14 takes precedence) · CPC title

• G01P1/006 Primary

  used for thermal compensation · CPC title

• G01P15/08 Primary

  with conversion into electric or magnetic values · CPC title

• B81B7/0019 Primary

  Protection against thermal alteration or destruction (B81B7/0083 takes precedence) · CPC title