Fault tolerant multidimensional acceleration and/or rotation sensor arrays with minimum numbers of redundant single dimension sensors and associated signal computation means

• US 8,127,606 B2
• Filed: 01/08/2009
• Issued: 03/06/2012
• Est. Priority Date: 01/11/2008
• Status: Expired due to Fees

• Current Assignee: Tenny Dahlin Lode
• Original Assignee: Tenny Dahlin Lode
• Inventors: Lode, Tenny Dahlin
• Primary Examiner(s): Williams, Hezron E
• Assistant Examiner(s): Shah, Samir M
• Application Number:
  US12/319,589
• Publication Number:
  US 20090178481A1
• Time in Patent Office: 1,153 Days
• Field of Search: 735/040.3, 735/03, 735/040.4, 735/041.2, 735/07, 735/10, 735/140.1, 735/140.2, 735/141.6, 73/13.7, 342/357.62
• US Class Current: 73/504.03
• CPC Class Codes: G01C 21/166 Mechanical, construction or arrangement details of inertial navigation systems
• CPC Class Codes: G01C 21/183 Compensation of inertial measurements, e.g. for temperature effects
• CPC Class Codes: G01P 15/00 Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration
• CPC Class Codes: G01P 21/00 Testing or calibrating of apparatus or devices covered by the preceding groups

Abstract

An inertial system design approach that can sense and tolerate failures of individual single dimensional acceleration and/or rotation sensors with a minimal number of sensors. Sets of 4 single dimensional acceleration and/or rotation sensors can provide full 3 dimensional sensing in spite of a sensor malfunction or failure, and sets of 3 single dimensional acceleration and/or rotation sensors can provide full 2 dimensional sensing in spite of a sensor malfunction or failure.

Claims

1. An inertial sensor system comprising:

a plurality of inertial measurement devices, said plurality comprising either accelerometers, rotation sensors or both;

each of said devices in said plurality capable of sensing an acceleration value or a rotation value along three different axes in substantially different directions, said acceleration or rotation values capable of being represented in vector form;

signal detection and analysis means for receiving data from each of said devices in said plurality and applying appropriate multiplication factors for one or more of said acceleration or rotation values to determine if a vector sum of one or more acceleration or rotation values has a zero or near-zero vector value; and

wherein said signal detection and analysis means correlates a significant non-zero vector value with a failure or malfunction in one or more inertial measurement devices.

2. The system of claim 1, wherein an occurrence of a significant non-zero vector value in conjunction with its being parallel with a sensing axis of an inertial measurement device identifies the inertial measurement device which has failed or malfunctioned.

3. The system of claim 1, wherein an occurrence of a significant non-zero vector value in conjunction with its not being parallel with a sensing axis of any one inertial measurement device identifies the two or more inertial measurement devices which have failed or malfunctioned.

4. An inertial sensor system comprising:

a grouping of inertial measurement devices that form a set of three accelerometers, a set of three rotation sensors or a set of three accelerometers and three rotation sensors, the devices in a grouping capable of sensing an acceleration value or rotation value along three different axes in substantially different directions, the sensed acceleration or rotation values capable of being represented in vector form;

a signal detection and analysis means for receiving said sensed acceleration or rotation values from each of said devices in a grouping and determining if a vector sum of said sensed acceleration or rotation values has a zero or near-zero vector value; and

said signal detection and analysis means determining that a significant non-zero vector value indicates a malfunction in at least one of the devices in a grouping and allowing the system to continue to operate if two devices in a grouping remain functional.

5. The system of claim 4, wherein an occurrence of a significant non-zero vector value in conjunction with its being parallel with a sensing axis of an inertial measurement device identifies the inertial measurement device which has failed or malfunctioned.

6. The system of claim 4, wherein an occurrence of a significant non-zero vector value in conjunction with its not being parallel with a sensing axis of any one inertial measurement device identifies the two or more inertial measurement devices which have failed or malfunctioned.

7. An inertial sensor system comprising:

a grouped set of at least four accelerometers, a grouped set of at least four rotation sensors or a grouped set of at least four accelerometers and at least four rotation sensors, the accelerometers or rotation sensors in a grouped set capable of sensing an acceleration value or rotation value along three different axes in substantially different directions, the sensed acceleration or rotation values capable of being represented in vector form;

a signal detection and analysis means for receiving said sensed acceleration or rotation values from each of the accelerometers or rotation sensors in a grouped set and determining if a vector sum of said sensed acceleration or rotation values has a zero or near-zero vector value; and

said signal detection and analysis means determining that a significant non-zero vector value indicates a malfunction in at least one of the accelerometers or rotation sensors in a grouped set and allowing the system to continue to operate if at least two accelerometers or at least two rotation sensors in a grouped set remain functional.

8. The system of claim 7, wherein an occurrence of a significant non-zero vector value in conjunction with its being parallel with a sensing axis of an accelerometer or rotation sensor in a grouped set identifies the accelerometer or rotation sensor which has failed or malfunctioned.

9. The system of claim 7, wherein an occurrence of a significant non-zero vector value in conjunction with its not being parallel with a sensing axis of any one accelerometer or rotation sensor in a grouped set identifies the two or more accelerometers or rotation sensors which have failed or malfunctioned.