Classifications

• • G—PHYSICS
  • G01—MEASURING; TESTING
  • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
  • G01P15/00—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration
  • G01P15/02—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses
  • G01P15/08—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values
  • G01P15/13—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values by measuring the force required to restore a proofmass subjected to inertial forces to a null position
• • G—PHYSICS
  • G01—MEASURING; TESTING
  • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
  • G01P15/00—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration
  • G01P15/02—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses
  • G01P15/08—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values
  • G01P15/13—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values by measuring the force required to restore a proofmass subjected to inertial forces to a null position
  • G01P15/132—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values by measuring the force required to restore a proofmass subjected to inertial forces to a null position with electromagnetic counterbalancing means

Definitions

• This invention relates to a measuring instrument, as a servoed accelerometer, with a digital output.
• Typical accelerometers have an analog output of current, voltage or frequency.
• the analog signal In order to interface such an instrument with a digital computer, the analog signal must be converted to digital form. For the current and voltage instruments, this is generally accomplished with an analog-to-frequency converter.
• a computer or other frequency measurement In the case of a frequency output accelerometer or a voltage-to-frequency conversion, a computer or other frequency measurement is required to generate a digital output.
• a frequency output accelerometer or a voltage-to-frequency conversion a computer or other frequency measurement is required to generate a digital output.
• an open loop configuration such an instrument is nonlinear.
• the output In a closed loop instrument, the output has a high noise level and different scale factors for positive and negative inputs.
• a servoed instrument has a displaceable element with means for applying force to the element to return the element to its null position.
• a detector responsive to displacement of the element from the null position has an analog output signal with a polarity which indicates the direction of displacement and an amplitude which represents the magnitude of the displacement.
• An analog-to-digital converter is responsive to the detector output signal and has a digital output representing the sensed stimulus to which the element responds.
• a digital-to-analog converter has an input connected with the output of the analog-to- digital converter and an analog output connected with the displacement element forcer to return the element to the null position. The digital output of the analog-to- digital converter provides an instrument output which is computer compatible.
• the analog-to-digital converter is an accumulator, the output of which is one-half full count for a null condition in the absence of a stimulus acting on the displacement element and which increments for one polarity of detector output signal and decrements for the opposite polarity of detector output signal.
• the digital-to-analog converter has a bipolar analog output which is zero for one-half full scale digital input.
• Accelerometer 10 has a proof mass element 11 connected by a hinge section 12 with a base 13. Proof mass 11 is displaceable in opposite directions from its null or rest position in response to an acceleration having a component in the direction of double ended arrow 14. Movement of the element 11 is sensed as by the differential capacitors including plates 15, 16 and a plate (not shown) on displaceable element 11. A restoring force is applied to the displaceable element by a current flow through coils 17, 18. The generation of restoring current will be described below. Further details of such an accelerometer may be found in Jacobs U.S. patent 3,702,073.
• a detector circuit 20 connected with capacitor plates 15, 16 has an analog output signal with a polarity which indicates the direction of displacement of element 11 and an amplitude which represents the magnitude of the displacement or other sensed stimulus.
• the detector output signal is connected with the input of an up-down accumulator 21 which increments for one polarity of detector output signal and decrements for the other polarity of detector output signal.
• An amplifier 22 may be connected between detector 20 and accumulator 21 to scale the analog signal, provide isolation between the detector and the accumulator and to provide frequency compensation should that be desirable.
• Up-down accumulator 21 as shown in the drawing has a 16 bit output which provides a binary digital output representing the stimulus acting on the displaceable element 11.
• the accumulator output is nominally one-half full count for a null condition of the displaceable element 11, e.g., the absence of an acceleration.
• the binary digital output may be buffered to provide the appropriate signal amplitude and isolation.
• the buffer output is typically connected with a computer or other digital signal processing equipment.
• the output of up-down accumulator 21 is also connected with the input of a bipolar digital-to-analog converter 25 which has a zero output for a half count of the 16 input bits.
• the analog output of digital-to-analog converter 25 is connected with forcer coils 17, 18 to return displaceable element to a null position.
• Appropriate clock inputs are provided to the accumulator 21 and digital-to-analog converter 25.
• Amplifier 26 may be connected between the output of digital-to-analog converter 25 and forcer coils 17, 18 to scale the current to the coils and provide frequency compensation.
• the analog output of detector 20 causes accumulator 21 to count up or down.
• the digital-to-analog converter 25 develops an analog rebalance current which returns the displaceable element 11 to its null position.
• Accumulator 21 has a low noise output which is directly compatible with a digital computer. Null or zero input bias errors can be compensated in the buffer circuit by incorporating an add or subtract count circuit. As the instrument is designed to interface with a digital computer, this bias correction can also be provided by adding or subtracting counts in subsequent processing.
• the rebalance current typically required will be between counts of the accumulator and steps of the digital-to-analog converter 25.
• the 16 bit accumulator shown in the drawing provides a 16 bit output resolution which is approximately 1/4 mG in a 20G full range accelerometer.
• the two least significant bits of the binary digital output may be suppressed to avoid instability in the digital output, or the readings may be sampled and averaged to increase resolution beyond the nominal 1635 bits. Since the servo loop forces the detector output to average zero over time, the LSB will be duty cycled to average proportionately between steps.
• the accumulator and digital-to- analog converter outputs will rattle or switch back and forth the least significant bits. This does not affect the binary digital output. It has a beneficial effect with an instrument having a pivot and jewel mount rather than hinge shown in the drawing, in causing the displaceable element to dither about the null position. This reduces hysteresis and nonrepeatability errors.
• Aliasing is an error which occurs when an instrument is read by a computer. Output changes are apparent to the computer only at transitions of the computer's clock. Normally the output of the instrument will change at some time other than the computer clock transition. If the time to a negative going output change of the instrument is 10.5 computer clock cycles, the time will appear to the computer as 10 clock cycles. If the time to the next positive going change is also 10.5 clock cycles it will appear to the computer as 11 clock cycles. If changes continue at this rate (some fraction of the computer clock rate) this gives an error in the apparent average output the computer sees.
• This instrument may be syncronized with a system clock so that output transitions can occur only after an integer number of computer clock cycles. This eliminates aliasing and does not increase the average error, since if one transition is delayed, the error is stored as failure to totally rebalance the pendulum and some subsequent transition of this same polarity will occur sooner.

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• Physics & Mathematics (AREA)
• General Physics & Mathematics (AREA)
• Electromagnetism (AREA)
• Length Measuring Devices With Unspecified Measuring Means (AREA)
• Force Measurement Appropriate To Specific Purposes (AREA)
• Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
• Feedback Control In General (AREA)
• Oscillators With Electromechanical Resonators (AREA)
• Input Circuits Of Receivers And Coupling Of Receivers And Audio Equipment (AREA)
• Optical Record Carriers And Manufacture Thereof (AREA)

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• 1985
  • 1985-06-10 IL IL75470A patent/IL75470A0/xx unknown
  • 1985-06-17 EP EP85903164A patent/EP0190165A1/en not_active Withdrawn
  • 1985-06-17 DE DE19853590290 patent/DE3590290T1/de not_active Ceased
  • 1985-06-17 WO PCT/US1985/001143 patent/WO1986000416A1/en not_active Application Discontinuation
  • 1985-06-17 GB GB08603995A patent/GB2169717A/en not_active Withdrawn
  • 1985-06-17 AU AU44918/85A patent/AU4491885A/en not_active Abandoned
  • 1985-06-17 KR KR1019860700095A patent/KR860700292A/ko not_active Application Discontinuation
  • 1985-06-17 JP JP60502709A patent/JPS61502489A/ja active Pending
  • 1985-06-18 IT IT48235/85A patent/IT1184278B/it active
• 1986
  • 1986-02-18 NO NO860609A patent/NO860609L/no unknown

Non-Patent Citations (1)

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