WO2021193597A1 - 方位角姿勢角計測装置 - Google Patents
方位角姿勢角計測装置 Download PDFInfo
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- WO2021193597A1 WO2021193597A1 PCT/JP2021/011897 JP2021011897W WO2021193597A1 WO 2021193597 A1 WO2021193597 A1 WO 2021193597A1 JP 2021011897 W JP2021011897 W JP 2021011897W WO 2021193597 A1 WO2021193597 A1 WO 2021193597A1
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- angular velocity
- velocity sensor
- control circuit
- side control
- vibration
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- 230000006870 function Effects 0.000 claims abstract description 137
- 238000001514 detection method Methods 0.000 claims description 54
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- 238000000034 method Methods 0.000 description 11
- 230000001360 synchronised effect Effects 0.000 description 6
- 238000010586 diagram Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 239000003990 capacitor Substances 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000007274 generation of a signal involved in cell-cell signaling Effects 0.000 description 1
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
- G01C19/56—Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces
- G01C19/5719—Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces using planar vibrating masses driven in a translation vibration along an axis
- G01C19/5726—Signal processing
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
- G01C21/10—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
- G01C21/12—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
- G01C21/16—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C17/00—Compasses; Devices for ascertaining true or magnetic north for navigation or surveying purposes
- G01C17/02—Magnetic compasses
- G01C17/28—Electromagnetic compasses
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
- G01C19/56—Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces
- G01C19/5705—Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces using masses driven in reciprocating rotary motion about an axis
- G01C19/5712—Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces using masses driven in reciprocating rotary motion about an axis the devices involving a micromechanical structure
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
- G01C19/56—Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces
- G01C19/5719—Turn-sensitive devices using vibrating masses, e.g. vibratory angular rate sensors based on Coriolis forces using planar vibrating masses driven in a translation vibration along an axis
- G01C19/5733—Structural details or topology
- G01C19/5755—Structural details or topology the devices having a single sensing mass
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C25/00—Manufacturing, calibrating, cleaning, or repairing instruments or devices referred to in the other groups of this subclass
- G01C25/005—Manufacturing, calibrating, cleaning, or repairing instruments or devices referred to in the other groups of this subclass initial alignment, calibration or starting-up of inertial devices
Definitions
- the present invention relates to an azimuth / attitude angle measuring device, and more particularly to an azimuth / attitude angle measuring device including a plurality of angular velocity sensors.
- an azimuth / attitude angle measuring device equipped with a plurality of angular velocity sensors is known.
- the above-mentioned Japanese Patent Application Laid-Open No. 2009-115559 discloses an electronic device (azimuth angle / attitude angle measuring device) including a plurality of angular velocity sensors.
- a ring-shaped element portion and a plurality of electrodes are arranged radially outside the ring-shaped element portion and in a circumferential shape.
- the plurality of electrodes include a primary electrode and a secondary electrode.
- An AC power source that generates primary vibration is connected to the ring-shaped element portion by applying an AC voltage to one of the primary electrode and the secondary electrode to one of the primary electrode and the secondary electrode. ing.
- a detecting means for detecting the magnitude of an electric signal generated in the other of the primary electrode and the secondary electrode is connected to the other of the primary electrode and the secondary electrode. Then, when the primary vibration is generated in the ring-shaped element portion and the rotational motion is generated in the normal direction of the element portion, the secondary vibration corresponding to the angular velocity of the rotational motion is generated in the element portion. Then, the magnitude of the electric signal generated on the other of the primary electrode and the secondary electrode due to the secondary vibration is detected by the detection means connected to the other of the primary electrode and the secondary electrode. Will be done. Further, based on the magnitude of the detected electric signal, an AC voltage for canceling the secondary vibration is applied to one of the primary electrode and the secondary electrode. Then, the magnitude of the angular velocity is calculated based on the magnitude of the AC voltage for canceling the secondary vibration.
- the angular velocity detected by the angular velocity sensor contains a bias component.
- the bias component is caused by the asymmetry of the gyro element included in the angular velocity sensor. Therefore, in a conventional angular velocity sensor such as Japanese Patent Application Laid-Open No. 2009-115559, an electrode to which an AC power supply is connected (one of a primary electrode and a secondary electrode) and an electrode to which a detection means is connected are connected. It is configured to cancel the bias component by switching (the other of the primary electrode and the secondary electrode) and differentizing the outputs of the angular velocity sensors before and after the switching.
- an electrode to which an AC power supply is connected one of a primary electrode and a secondary electrode
- an electrode to which a detection means is connected are connected.
- the bias component is canceled by switching (the other of the primary electrode and the secondary electrode) and differentizing the outputs of the angular velocity sensors before and after the switching. Therefore, in the azimuth angle attitude angle measuring device provided with a plurality of angular velocity sensors, in order to cancel the bias component of one angular velocity sensor, one of the electrodes (one of the primary electrode and the secondary electrode) to which the AC power supply is connected is connected.
- the electrode to which the detection means is connected (the other of the primary electrode and the secondary electrode)
- the power fluctuation of the AC power supply occurs.
- the present invention has been made to solve the above-mentioned problems, and one object of the present invention is to accurately detect an angular velocity in each of a plurality of angular velocity sensors connected to a common power supply unit. It is to provide a vibrating angular velocity sensor capable of.
- the azimuth angle attitude angle measuring device includes a first angular velocity sensor that detects an angular velocity around the first axis and a second axis in a direction different from the first axis.
- the first angle speed sensor and the second angle speed sensor include a second angle speed sensor that detects the ambient angular speed, a power supply unit that supplies power to the first angle speed sensor and the second angle speed sensor, and a control unit.
- a primary control circuit that has a closed control loop and the output of the closed control loop induces primary vibration in the transducer, and an angular velocity applied to the transducer that causes the transducer to generate 2
- the function as a circuit can be exchanged, and the control unit is configured before and after exchanging the functions of the primary side control circuit and the secondary side control circuit in one of the first angle speed sensor and the second angle speed sensor.
- the angular velocity for use in the calculation is detected in, the other of the first angular velocity sensor and the second angular velocity sensor does not perform control to switch the functions of the primary side control circuit and the secondary side control circuit. It is configured as follows.
- the azimuth angle / attitude angle measuring device has the functions of the primary side control circuit and the secondary side control circuit in one of the first angular velocity sensor and the second angular velocity sensor. Control to switch the functions of the primary side control circuit and the secondary side control circuit in the other of the first angular velocity sensor and the second angular velocity sensor when the angular velocity to be used for the calculation is detected before and after the replacement of.
- a control unit is provided so as not to perform the above.
- the other of the first angular velocity sensor and the second angular velocity sensor detects the angular velocity to be used for the calculation
- the other of the first angular velocity sensor and the second angular velocity sensor has the primary side control circuit and the secondary side. Since the functions of the control circuit are not exchanged, the power of the power supply unit provided in common does not change due to the exchange of the functions of the primary side control circuit and the secondary side control circuit. As a result, power is stably supplied from the power supply unit to one of the first angular velocity sensor and the second angular velocity sensor, so that the angular velocity for use in the calculation can be detected accurately. As a result, the angular velocity can be accurately detected in each of the plurality of angular velocity sensors connected to the common power supply unit.
- the control unit has the detection result of the angular velocity in which the secondary vibration of the vibrator is detected by the secondary side control circuit, and the primary side control circuit and the secondary side.
- the angular velocity bias detected by the first angular velocity sensor and the second angular velocity sensor based on the detection result of the angular velocity in which the secondary vibration of the vibrator is detected by the primary side control circuit by exchanging the functions with the side control circuit. It is configured to perform an operation that cancels a component. With this configuration, the bias component of the angular velocity detected by the first angular velocity sensor and the second angular velocity sensor can be accurately calculated based on the angular velocity detected while the power is stably supplied from the power supply unit. can.
- the control unit is configured to suspend the detection of the angular velocity for canceling the bias component of the angular velocity for a predetermined period before and after switching the functions of the primary side control circuit and the secondary side control circuit.
- the angular velocity is detected to cancel the angular velocity bias component during the period when the power of the power supply unit fluctuates due to the replacement of the functions of the primary side control circuit and the secondary side control circuit. Is interrupted, so that it is possible to effectively suppress a decrease in the detection accuracy of the angular velocity for use in the calculation for canceling the bias component.
- the control unit functions as a primary side control circuit and a secondary side control circuit in one of the first angular velocity sensor and the second angular velocity sensor.
- Is configured to perform control for switching the functions of the primary side control circuit and the secondary side control circuit in the other of the first angular velocity sensor and the second angular velocity sensor in a predetermined period before and after the replacement.
- control unit is configured so that the timing of switching the functions of the primary side control circuit and the secondary side control circuit in the first angular velocity sensor and the second angular velocity sensor is substantially the same.
- a third angular velocity sensor including an oscillator and detecting an angular velocity around the first axis
- the power supply unit includes a first angular velocity sensor and a second angular velocity sensor.
- the control unit detects the angular velocity to be used for calculation in the third angular velocity sensor, the first angular velocity sensor.
- the control is configured so that the functions of the primary side control circuit and the secondary side control circuit are not exchanged.
- the third angular velocity sensor can also accurately detect the angular velocity to be used for calculation. Can be done.
- the azimuth angle attitude angle measuring device has a first angular velocity sensor that detects an angular velocity around the first axis and a second angular velocity that detects an angular velocity around the second axis in a direction different from the first axis. It includes an angular velocity sensor, a power supply unit that supplies power to the first angular velocity sensor and the second angular velocity sensor, and a control unit.
- the first angular velocity sensor and the second angular velocity sensor have an oscillator and a closed control loop. Then, the output of the closed control loop induces the primary vibration in the vibrator, and the closed control that detects the secondary vibration generated in the vibrator due to the angular velocity applied to the vibrator.
- Each of the secondary control circuits having a loop is included, and the function of inducing the primary vibration and the function of detecting the secondary vibration are interchangeably configured, and the control unit includes the first angular velocity sensor and the second angular velocity sensor.
- the first angular velocity sensor and the second angular velocity detects the angular velocity to be used for calculation before and after switching the function of inducing the primary vibration and the function of detecting the secondary vibration
- the first angular velocity sensor and the second angular velocity The other of the sensors is configured not to perform control to switch between the function of inducing the primary vibration and the function of detecting the secondary vibration.
- the azimuth angle / attitude angle measuring device detects the function of inducing the primary vibration and the secondary vibration in one of the first angular velocity sensor and the second angular velocity sensor.
- the function of inducing the primary vibration and the function of detecting the secondary vibration in the other of the first angular velocity sensor and the second angular velocity sensor is replaced.
- a control unit is provided so as not to perform control for exchanging and.
- the control unit detects the detection result of the angular velocity at which the secondary vibration of the vibrator is detected, the function of inducing the primary vibration, and the secondary vibration. Based on the detection result of the angular velocity that detects the secondary vibration of the vibrator by exchanging the functions, the calculation is configured to cancel the bias component of the angular velocity detected by the first angular velocity sensor and the second angular velocity sensor. ing. With this configuration, the bias component of the angular velocity detected by the first angular velocity sensor and the second angular velocity sensor can be accurately calculated based on the angular velocity detected while the power is stably supplied from the power supply unit. can.
- the control unit interrupts the detection of the angular velocity for canceling the bias component of the angular velocity for a predetermined period before and after switching the function of inducing the primary vibration and the function of detecting the secondary vibration. It is configured in. With this configuration, the angular velocity for canceling the bias component of the angular velocity during the period when the power fluctuation of the power supply unit occurs due to the replacement of the function of inducing the primary vibration and the function of detecting the secondary vibration. Since the detection of the angular velocity is interrupted, it is possible to effectively suppress a decrease in the detection accuracy of the angular velocity for use in the calculation for canceling the bias component.
- the control unit detects the function of inducing the primary vibration and the secondary vibration in one of the first angular velocity sensor and the second angular velocity sensor. It is configured to control the switching between the function of inducing the primary vibration and the function of detecting the secondary vibration in the other of the first angular velocity sensor and the second angular velocity sensor in a predetermined period before and after the replacement of the functions. ing. With this configuration, the timing to switch the function of inducing the primary vibration of the first angular velocity sensor and the function of detecting the secondary vibration, the function of inducing the primary vibration of the second angular velocity sensor, and the secondary vibration can be obtained.
- the timing for replacing the detection function can be performed during a predetermined period during which the detection of the angular velocity for canceling the bias component of the angular velocity is interrupted.
- control unit is configured so that the timing of switching the function of inducing the primary vibration and the function of detecting the secondary vibration in the first angular velocity sensor and the second angular velocity sensor is substantially the same. ..
- a third angular velocity sensor including a vibrator and detecting an angular velocity around the first axis
- the power supply unit includes a first angular velocity sensor and a second angular velocity sensor.
- the control unit detects the angular velocity to be used for calculation in the third angular velocity sensor, the first angular velocity sensor.
- the third angular velocity sensor can also accurately detect the angular velocity to be used for calculation. Can be done.
- the angular velocity can be accurately detected in each of the plurality of angular velocity sensors connected to the common power supply unit.
- the azimuth angle attitude measuring device 100 is configured to detect the azimuth angle and the attitude angle. Specifically, the azimuth / attitude angle measuring device 100 detects angular velocities around the X-axis, Y-axis, and Z-axis that are orthogonal to each other, and based on the detected angular velocities, the three-dimensional azimuth and attitude angles. Is configured to detect.
- the azimuth / attitude angle measuring device 100 includes a control unit 101, a power supply unit 102, an angular velocity sensor 103, an angular velocity sensor 104, and an angular velocity sensor 105.
- the angular velocity sensor 103, the angular velocity sensor 104, and the angular velocity sensor 105 are configured to detect angular velocities around axes that intersect each other.
- the angular velocity sensor 103 is configured to detect the angular velocity around the X-axis.
- the angular velocity sensor 104 is configured to detect the angular velocity around the Y-axis.
- the angular velocity sensor 105 is configured to detect the angular velocity around the Z axis. That is, the angular velocity sensor 103, the angular velocity sensor 104, and the angular velocity sensor 105 are configured to detect the angular velocities around the axes orthogonal to each other.
- the angular velocity sensor 103 is an example of the "first angular velocity sensor” in the claims.
- the angular velocity sensor 104 is an example of the "second angular velocity sensor” in the claims.
- the angular velocity sensor 105 is an example of the "second angular velocity sensor” in the claims.
- the control unit 101 is configured to control each unit of the azimuth / posture angle measuring device 100.
- the control unit 101 includes a CPU (CENTRAL PROCESSING UNIT) and a memory.
- the power supply unit 102 is configured to supply electric power to each unit of the azimuth angle attitude measuring device 100. Specifically, the power supply unit 102 is configured to supply electric power to the angular velocity sensors 103, 104, and 105. Further, the power supply unit 102 is configured to supply AC power to the angular velocity sensors 103, 104 and 105. The power supply unit 102 is configured to be supplied with electric power from an external power source or a battery provided in the azimuth / attitude angle measuring device 100. For example, the power supply unit 102 is a power conversion circuit that converts the supplied power. The power supply unit 102 includes a switching element, a capacitor, a diode, and the like.
- each of the angular velocity sensors 103, 104, and 105 has a vibrator 11 and a closed control loop, and the output of the closed control loop induces a primary vibration in the vibrator 11. It includes a side control circuit 12 and a secondary side control circuit 13 having a closed control loop that detects secondary vibrations generated in the vibrator 11 due to the angular velocity applied to the vibrator 11.
- the vibrator 11 includes a ring-shaped vibrator.
- the primary side control circuit 12 of the angular velocity sensor 103 includes an amplifier circuit 21, a synchronous detection circuit 22, a loop filter 23, a modulation circuit 24, and a drive circuit 25. It includes a PLL (Phase Locked Loop) circuit (phase-locked loop) 26 and a reference signal generation circuit 27.
- the oscillator 11, the amplifier circuit 21, the synchronous detection circuit 22, the loop filter 23, the modulation circuit 24, and the drive circuit 25 are connected in this order to form a closed control loop.
- the loop filter 23 includes, for example, an integral filter.
- FIG. 3 shows the configuration of the angular velocity sensor 103, the angular velocity sensors 104 and 105 also have the same configuration.
- the secondary side control circuit 13 of the angular velocity sensor 103 includes an amplifier circuit 31, a synchronous detection circuit 32, an addition circuit 33, a loop filter 34, a modulation circuit 35, a drive circuit 36, and an amplifier circuit. 37 and is included.
- the oscillator 11, the amplifier circuit 31, the synchronous detection circuit 32, the adder circuit 33, the loop filter 34, the modulation circuit 35, and the drive circuit 36 are connected in this order to form a closed control loop.
- the adder circuit 33 is composed of a general addition / subtraction circuit using an operational amplifier.
- the loop filter 34 includes, for example, an integral filter. Further, the output of the loop filter 34 is input to the amplifier circuit 37. Then, the signal output from the amplifier circuit 37 is output as the sensor output of the angular velocity sensors 103 (104, 105).
- the primary side control circuit 12 and the secondary side control circuit 13 of the angular velocity sensors 103 have a function as the primary side control circuit 12 and the secondary side control circuit 13. It is configured so that the functions as can be exchanged.
- a switch 41 is provided on the input side of the signal to the vibrator 11 and a switch 42 is provided on the output side of the signal to the vibrator 11 (output side of the amplifier circuit 21).
- a switch 43 is provided on the input side of the signal to the vibrator 11, and a switch 44 is provided on the output side of the signal to the vibrator 11 (the output side of the amplifier circuit 31).
- the switch 41, the switch 42, the switch 43, and the switch 44 are each configured to be able to switch between a state of being connected to the primary side control circuit 12 and a state of being connected to the secondary side control circuit 13. .
- the angular velocity sensors 103 (104, 105) are configured so that the function of inducing the primary vibration and the function of detecting the secondary vibration can be interchanged.
- the switch 41 and the switch 42 show the state of being connected to the primary side control circuit 12
- the switch 43 and the switch 44 show the state of being connected to the secondary side control circuit 13.
- the switch 41 and the switch 42 are switched so as to be connected to the secondary side control circuit 13
- the switch 43 and the switch 44 are switched so as to be connected to the primary side control circuit 12, so that the primary side control circuit 12 is connected.
- the function as the side control circuit 12 and the function as the secondary side control circuit 13 are interchanged with each other.
- the angular velocity sensors 103 are provided with an addition / subtraction amount adjusting circuit 14 to which an output from the primary side control circuit 12 (output from the loop filter 23) is input.
- the addition / subtraction amount adjusting circuit 14 adjusts the magnitude of the output of the loop filter 23 of the primary side control circuit 12 depending on the temperature, and adds the adjusted output (first offset value) to the secondary side control circuit 13. It is configured to be input to the circuit 33.
- the addition amount of the first offset value is adjusted by dividing the voltage using a potentiometer (volume resistor) or the like.
- the angular velocity sensors 103 (104, 105) are provided with an addition / subtraction amount adjusting circuit 15 to which a constant signal S1 independent of temperature is input.
- the addition / subtraction amount adjusting circuit 15 is configured to adjust the magnitude of the constant signal S1 and input the adjusted constant signal S1 (second offset value) to the addition circuit 33 of the secondary side control circuit 13. ing.
- the addition amount of a constant signal S1 is adjusted by dividing the voltage using a potentiometer (volume resistor) or the like.
- the control unit 101 is used for calculation before and after switching the functions of the primary side control circuit 12 and the secondary side control circuit 13 in any one of the angular velocity sensors 103 to 105.
- the other angular velocity sensors of the angular velocity sensors 103 to 105 are configured not to perform control for switching the functions of the primary side control circuit 12 and the secondary side control circuit 13. ing.
- the angular velocity sensors 103 (104, 105) always detect the angular velocity when the power is supplied from the power supply unit 102 and are driven, and output a signal based on the detected angular velocity.
- the control unit 101 is configured to calculate the attitude angle and the azimuth angle based on the signals output from the angular velocity sensors 103 (104, 105). Further, the control unit 101 is configured to perform an operation to calculate the bias component of the angular velocity sensor 103 (104, 105) based on the signal output from the angular velocity sensor 103 (104, 105).
- the control unit 101 uses the angular velocity detected by the other angular velocity sensors 103 to 105 for calculation when the functions of the primary side control circuit 12 and the secondary side control circuit 13 are exchanged in the angular velocity sensors 103 to 105. not present.
- control unit 101 detects the angular velocity detection result in which the secondary vibration of the vibrator 11 is detected by the secondary control circuit 13 of the angular velocity sensor 103 (104, 105), and the primary of the angular velocity sensor 103 (104, 105).
- the angular velocity sensor 103 (104) is based on the detection result of the angular velocity in which the secondary vibration of the vibrator 11 is detected by the primary side control circuit 12 by exchanging the functions of the side control circuit 12 and the secondary side control circuit 13. , 105) is configured to perform an operation to cancel the bias component of the angular velocity detected. Twice
- the control unit 101 detects the angular velocity at which the secondary vibration of the vibrator 11 is detected by the secondary control circuit 13 of the angular velocity sensor 103 during the period from time t1 to time t2 in FIG. 4A (A). get. Further, the control unit 101 detects (acquires) the angular velocity at which the secondary vibration of the vibrator 11 is detected by the primary side control circuit 12 of the angular velocity sensor 103 during the period from time t4 to time t5 in FIG. 4 (A). .. Then, the control unit 101 calculates the bias component of the angular velocity sensor 103 based on the angular velocity acquired in the period from time t1 to time t2 and the angular velocity acquired in the period from time t4 to time t5.
- control unit 101 acquires the angular velocity at which the secondary vibration of the vibrator 11 is detected by the secondary control circuit 13 of the angular velocity sensor 104 during the period from time t11 to time t12 in FIG. 4B for calculation. do. Further, the control unit 101 acquires the angular velocity at which the secondary vibration of the vibrator 11 is detected by the primary side control circuit 12 of the angular velocity sensor 104 for calculation in the period from the time t14 to the time t15 in FIG. 4 (B). do.
- control unit 101 calculates (calculates) the bias component of the angular velocity sensor 104 based on the angular velocity acquired in the period from time t11 to time t12 and the angular velocity acquired in the period from time t14 to time t15.
- control unit 101 acquires the angular velocity at which the secondary vibration of the vibrator 11 is detected by the secondary control circuit 13 of the angular velocity sensor 105 during the period from time t21 to time t22 in FIG. 4C for calculation. do. Further, the control unit 101 acquires the angular velocity at which the secondary vibration of the vibrator 11 is detected by the primary side control circuit 12 of the angular velocity sensor 105 for calculation in the period from the time t24 to the time t25 in FIG. 4C. do.
- control unit 101 calculates (calculates) the bias component of the angular velocity sensor 105 based on the angular velocity acquired in the period from time t21 to time t22 and the angular velocity acquired in the period from time t24 to time t25.
- control unit 101 receives the angular velocity of the angular velocity sensor 103 (104, 105) for a predetermined period before and after switching the functions of the primary side control circuit 12 and the secondary side control circuit 13 of the angular velocity sensor 103 (104, 105). It is configured to interrupt the detection of the angular velocity to cancel the bias component of. Specifically, a predetermined period (time t2 to time t4) before and after the timing (time t3) for switching the functions of the primary side control circuit 12 and the secondary side control circuit 13 of the angular velocity sensor 103 of FIG. 4 (A).
- the control unit 101 interrupts the detection (acquisition for calculation) of the angular velocity for canceling the bias component of the angular velocity of the angular velocity sensors 104 and 105. Further, in a predetermined period (period from time t12 to time t14) before and after the timing (time t13) in which the functions of the primary side control circuit 12 and the secondary side control circuit 13 of the angular velocity sensor 104 of FIG. 4B are exchanged. , The control unit 101 interrupts the detection (acquisition for calculation) of the angular velocity for canceling the bias component of the angular velocity of the angular velocity sensors 103 and 105.
- the control unit 101 interrupts the detection (acquisition for calculation) of the angular velocity for canceling the bias component of the angular velocity of the angular velocity sensors 103 and 104.
- control unit 101 is used in the other angular velocity sensors 103 to 105 during a predetermined period before and after switching the functions of the primary side control circuit 12 and the secondary side control circuit 13 in any of the angular velocity sensors 103 to 105. It is configured to perform control for exchanging the functions of the primary side control circuit 12 and the secondary side control circuit 13. Specifically, the control unit 101 has a predetermined period (time) before and after the timing (time t3) of switching the functions of the primary side control circuit 12 and the secondary side control circuit 13 of the angular velocity sensor 103 of FIG. 4 (A).
- the functions of the primary side control circuit 12 and the secondary side control circuit 13 of the angular velocity sensors 104 and 105 are exchanged.
- the control unit 101 has a predetermined period (time t12 to time) before and after the timing (time t13) for switching the functions of the primary side control circuit 12 and the secondary side control circuit 13 of the angular velocity sensor 104 of FIG. 4 (B).
- the functions of the primary side control circuit 12 and the secondary side control circuit 13 of the angular velocity sensors 103 and 105 are exchanged.
- control unit 101 has a predetermined period (time t22 to time) before and after the timing (time t23) for switching the functions of the primary side control circuit 12 and the secondary side control circuit 13 of the angular velocity sensor 105 of FIG. 4 (C). In the period of t24), the functions of the primary side control circuit 12 and the secondary side control circuit 13 of the angular velocity sensors 103 and 104 are exchanged.
- control unit 101 is configured so that the timing of switching the functions of the primary side control circuit 12 and the secondary side control circuit 13 in the angular velocity sensors 103, 104 and 105 is substantially simultaneous. That is, the control unit 101 sets the time t3 in FIG. 4 (A), the time t13 in FIG. 4 (B), and the time t23 in FIG. 4 (C) at the same timing, and sets the angular velocity sensors 103, 104, and 105. The functions of the primary side control circuit 12 and the secondary side control circuit 13 are exchanged.
- the angular velocity to be used for the calculation before and after the functions of the primary side control circuit 12 and the secondary side control circuit 13 are exchanged is determined.
- a control unit configured not to perform control for switching the functions of the primary side control circuit 12 and the secondary side control circuit 13 in the other angular velocity sensors among the angular velocity sensors 103 to 105 when detecting. Is provided.
- the functions of the primary side control circuit 12 and the secondary side control circuit 13 in the other angular velocity sensors 103 to 105 when any of the angular velocity sensors 103 to 105 detects the angular velocity to be used for the calculation, the functions of the primary side control circuit 12 and the secondary side control circuit 13 in the other angular velocity sensors 103 to 105.
- the power of the power supply unit 102 provided in common does not change due to the replacement of the functions of the primary side control circuit 12 and the secondary side control circuit 13.
- the power supply unit 102 stably supplies electric power to the angular velocity sensors 103 to 105, so that the angular velocity for use in the calculation can be detected with high accuracy.
- the angular velocity can be accurately detected in each of the plurality of angular velocity sensors 103 to 105 connected to the common power supply unit 102.
- the control unit 101 has the detection result of the angular velocity in which the secondary vibration of the vibrator 11 is detected by the secondary side control circuit 13, and the primary side control circuits 12 and secondary.
- the bias component of the angular velocity detected by the angular velocity sensors 103 to 105 based on the detection result of the angular velocity in which the secondary vibration of the vibrator 11 is detected by the primary side control circuit 12 by exchanging the functions with the side control circuit 13. Is configured to perform an operation that cancels.
- the bias component of the angular velocity detected by the angular velocity sensors 103 to 105 can be accurately calculated based on the angular velocity detected while the power is stably supplied from the power supply unit 102.
- the control unit 101 cancels the bias component of the angular velocity for a predetermined period before and after switching the functions of the primary side control circuit 12 and the secondary side control circuit 13. It is configured to interrupt the detection of the angular velocity of.
- the angular velocity for canceling the angular velocity bias component can be detected during the period in which the power of the power supply unit 102 fluctuates due to the replacement of the functions of the primary side control circuit 12 and the secondary side control circuit 13. Since it is interrupted, it is possible to effectively suppress a decrease in the detection accuracy of the angular velocity for use in the calculation for canceling the bias component.
- the control unit 101 is predetermined before and after the functions of the primary side control circuit 12 and the secondary side control circuit 13 in any of the angular velocity sensors 103 to 105 are exchanged.
- the other angular velocity sensors 103 to 105 are configured to perform control in which the functions of the primary side control circuit 12 and the secondary side control circuit 13 are exchanged.
- the timing of switching the functions of the primary side control circuit 12 and the secondary side control circuit 13 of the angular velocity sensors 103 to 105 is performed during a predetermined period during which the detection of the angular velocity for canceling the bias component of the angular velocity is interrupted. be able to.
- the angular velocity for canceling the bias component of the angular velocity is detected in parallel in a plurality of the angular velocity sensors 103 to 105, the angular velocity for use in the calculation can be detected with high accuracy.
- control unit 101 is configured to switch the functions of the primary side control circuit 12 and the secondary side control circuit 13 in the angular velocity sensors 103 to 105 substantially at the same time. Constitute. As a result, it is possible to minimize the predetermined period during which the detection of the angular velocity for canceling the bias component of the angular velocity is interrupted, so that the time for detecting the angular velocity for canceling the bias component becomes longer. It can be suppressed.
- the vibrator 11 includes a ring type vibrator.
- the ring-shaped vibrator has a symmetrical shape, the vibration mode by the primary side control circuit 12 and the vibration mode by the secondary side control circuit 13 are similar. As a result, it is not necessary to consider the influence of the difference in the vibration modes of the angular velocity sensors 103 to 105 including the ring type vibrator 11.
- the function for inducing the primary vibration and the function for detecting the secondary vibration are used for calculation before and after switching.
- the other angular velocity sensors among the angular velocity sensors 103 to 105 are configured not to perform control to switch the function of inducing the primary vibration and the function of detecting the secondary vibration.
- a control unit is provided.
- the power supply unit 102 stably supplies electric power to the angular velocity sensors 103 to 105, so that the angular velocity for use in the calculation can be detected with high accuracy. As a result, the angular velocity can be accurately detected in each of the plurality of angular velocity sensors 103 to 105 connected to the common power supply unit 102.
- the azimuth angle attitude angle measuring device 200 includes a control unit 101, a power supply unit 102, an angular velocity sensor 103a, an angular velocity sensor 103b, an angular velocity sensor 104a, an angular velocity sensor 104b, and an angular velocity sensor 105a. It includes an angular velocity sensor 105b.
- the angular velocity sensors 103a and 103b, the angular velocity sensors 104a and 104b, and the angular velocity sensors 105a and 105b are configured to detect angular velocities around axes that intersect each other.
- the angular velocity sensors 103a and 103b are configured to detect the angular velocity around the axis parallel to or coaxial with each other. Further, the angular velocity sensors 104a and 104b are configured to detect angular velocities around axes parallel to or coaxial with each other. Further, the angular velocity sensors 105a and 105b are configured to detect the angular velocity around the axis parallel to or coaxial with each other.
- the angular velocity sensors 103a and 103b are configured to detect the angular velocity around the X-axis. Further, the angular velocity sensors 104a and 104b are configured to detect the angular velocity around the Y-axis. Further, the angular velocity sensors 105a and 105b are configured to detect the angular velocity around the Z axis. The angular velocity sensors 103a and 103b are arranged adjacent to each other. Further, the angular velocity sensors 104a and 104b are arranged adjacent to each other. Further, the angular velocity sensors 105a and 105b are arranged adjacent to each other.
- the angular velocity sensor 103a is an example of the "first angular velocity sensor” in the claims. Further, the angular velocity sensor 103b is an example of the “third angular velocity sensor” in the claims. Further, the angular velocity sensor 104a is an example of the “second angular velocity sensor” in the claims. Further, the angular velocity sensor 105a is an example of the “second angular velocity sensor” in the claims.
- the power supply unit 102 is configured to supply electric power to the angular velocity sensors 103a, 103b, 104a, 104b, 105a and 105b. Further, the power supply unit 102 is configured to supply AC power to the angular velocity sensors 103a, 103b, 104a, 104b, 105a and 105b.
- the control unit 101 functions as the primary side control circuit 12 and the secondary side control circuit 13 in any one of the angular velocity sensors 103a, 103b, 104a, 104b, 105a and 105b.
- the primary side control circuit 12 and the secondary side It is configured so as not to perform control for exchanging the function with the control circuit 13.
- the control unit 101 controls the angular velocity sensor 103a to switch the functions of the primary side control circuit 12 and the secondary side control circuit 13. Is configured not to do.
- the control unit 101 detects the angular velocity based on the secondary vibration of the vibrator 11 by the secondary side control circuit 13 in a predetermined period by the angular velocity sensor 103a, and the primary side control circuit.
- the functions of the 12 and the secondary side control circuit 13 are exchanged, and the primary side control circuit 12 is configured to perform a process of detecting an angular velocity based on the secondary vibration of the vibrator 11.
- the oscillator 11 is operated by the secondary control circuit 13 of the angular velocity sensor 103a during a predetermined period from time t31 to time t32 and from time t34 to time t35.
- a process of detecting the angular velocity based on the secondary vibration and a process of detecting the angular velocity based on the secondary vibration of the vibrator 11 by the primary side control circuit 12 of the angular velocity sensor 103a are performed.
- control unit 101 is configured to control the angular velocity sensor 103b to perform a process of detecting the angular velocity in a predetermined period. Specifically, as shown in FIG. 7B, during a predetermined period from time t31 to time t32 and from time t34 to time t35, the oscillator 11 is operated by the secondary control circuit 13 of the angular velocity sensor 103b. A process for detecting the angular velocity based on the secondary vibration is performed.
- control unit 101 has a bias component (B1 (t)) of the angular velocity sensor 103b based on the first detection result detected by the angular velocity sensor 103b in the predetermined period and the second detection result detected by the angular velocity sensor 103a in the predetermined period. )) Is configured to be calculated.
- control unit 101 subtracts the value of the second detection result detected by the angular velocity sensor 103a in the predetermined period from the value of the first detection result detected by the angular velocity sensor 103b in the predetermined period, thereby causing the bias component of the angular velocity sensor 103b. Is configured to calculate.
- the predetermined period includes a first period (a period from time t31 to time t32) in which the secondary side control circuit 13 detects the angular velocity based on the secondary vibration of the vibrator 11, and the primary side control circuit 12
- the first period and the second period are the same length of time. As shown in FIG. 7, each of the first period and the second period has a length of time T.
- the first detection result is an integral value of the angular velocity detected by the angular velocity sensor 103b in a predetermined period.
- the second detection result is an integral value of the angular velocity detected by the angular velocity sensor 103a in a predetermined period.
- the predetermined period is a period in which the bias component of the angular velocity sensor 103a is substantially constant.
- the predetermined period has a length of about several seconds to several tens of seconds.
- the predetermined period is a period in which the influence of the temperature change can be ignored and it can be assumed that the bias component of the angular velocity sensor 103a does not change substantially.
- the integral value I1 of the first detection result in the predetermined period (first period from time t31 to time t32 and second period from time t34 to time t35) shown in FIG. 7B is given by the equation (1). It is expressed as.
- the angular velocity ⁇ 1 (t) detected by the secondary control circuit 13 of the angular velocity sensor 103b is the angular velocity (true angular velocity) ⁇ 0 (t) generated by the motion (movement) shown in FIG. 7A and the angular velocity sensor 103b. It is expressed as in Eq. (2) using the bias B1 (t).
- the integrated value I2 of the second detection result in the predetermined period (the first period from the time t31 to the time t32 and the second period from the time t34 to the time t35) shown in FIG. 7C is expressed by the formula (C). It is expressed as 4).
- the integrated value is subtracted in consideration of the fact that ⁇ 2 (t) is inverted with respect to the bias component.
- the angular velocity ⁇ 2 (t) detected by the secondary side control circuit 13 of the angular velocity sensor 103a and the angular velocity ⁇ 2 (t) detected by the primary side control circuit 12 are the angular velocities generated by the motion (movement) shown in FIG. 7 (A).
- the true angular velocity) ⁇ 0 (t) and the bias B2 (t) of the angular velocity sensor 103a they are expressed as equations (5) and (6), respectively.
- equation (6) of the second period from the time t34 to the time t35 ⁇ 0 (t) is inverted with respect to the bias component, so that a minus is applied.
- the bias B1 (t) of the angular velocity sensor 103b and the bias B2 (t) of the angular velocity sensor 103a are Since the amount of change over time is negligible (because it is constant), it can be assumed that Eqs. (9) and (10) hold.
- B1 is the bias value of the angular velocity sensor 103b in the first period and the second period
- B2 is the bias value of the angular velocity sensor 103a in the first period and the second period.
- the bias value B1 of the angular velocity sensor 103b is calculated by dividing (I1-I2) by 2T.
- the calculated bias value B1 is used for detecting the angular velocity by the angular velocity sensor 103b. For example, it is used as an observation update of the Kalman filter.
- the equation is performed during the period in which the function of the angular velocity sensor 103a as the primary side control circuit 12 and the function of the secondary side control circuit 13 are exchanged and the angular velocity is measured to calculate the bias value B1. It suffices if the relationship between (9) and equation (10) is established. Therefore, for example, even if the time interval (t36-t35) up to the time t36, which is the start point of the next processing, is large and B1 changes, it can be similarly corrected by the processing from the next time t36. However, it is always preferable that the time interval (t36-t35) is sufficiently small in order to reduce the change in B1.
- the control unit 101 uses the angular velocity sensor 103b based on the first detection result detected by the angular velocity sensor 103b in the first predetermined period and the second detection result detected by the angular velocity sensor 103a in the first predetermined period. Calculate the bias component. Further, the control unit 101 calculates the bias component of the angular velocity sensor 103a by using the angular velocity detected by the angular velocity sensor 103a in the second predetermined period and the bias component of the angular velocity sensor 103b. Then, the control unit 101 alternately repeats these controls. That is, the bias component B1 of the angular velocity sensor 103b is corrected by calculating the first bias component.
- the corrected B1 is used to calculate ⁇ of B2, which is a bias component of the angular velocity sensor 103a. Then, in the next cycle, the corrected ⁇ is used to correct B1 which is a bias component of the angular velocity sensor 103b. After that, these processes are repeated alternately.
- the process of calculating and canceling the bias components of the angular velocity sensors 104a and 104b is the same as the process of calculating and canceling the bias components of the angular velocity sensors 103a and 103b. Further, the process of calculating and canceling the bias components of the angular velocity sensors 105a and 105b is the same as the process of calculating and canceling the bias components of the angular velocity sensors 103a and 103b.
- the angular velocity sensors 103a, 103b, 104a, 104b, 105a and 105b are stably supplied with electric power from the power supply unit 102, so that the angular velocity is used for calculation. Can be detected accurately. As a result, the angular velocity can be accurately detected in each of the plurality of angular velocity sensors 103a, 103b, 104a, 104b, 105a and 105b connected to the common power supply unit 102.
- the angular velocity sensor 103a when the angular velocity sensor 103b detects the angular velocity to be used for the calculation, the angular velocity sensor 103a has the primary side control circuits 12 and 2. It is configured so that the control for exchanging the function with the next control circuit 13 is not performed. Thereby, in the configuration provided with the angular velocity sensor 103a and the angular velocity sensor 103b for detecting the angular velocity around the same axis, the angular velocity for use in the calculation can be accurately detected by the angular velocity sensor 103b as well.
- the vibrator may have a symmetrical shape, and a disc type, a cup type (wine glass type), an octagonal type, or the like may be used.
- a closed control loop is configured by an oscillator, an amplifier circuit, a synchronous detection circuit, a loop filter, a modulation circuit and a drive circuit.
- the control loop may be configured by a configuration other than the configuration including an amplifier circuit, a synchronous detection circuit, a loop filter, a modulation circuit, and a drive circuit.
- an integral filter is used as the loop filter
- a loop filter other than the integral filter may be used.
- the angular velocity sensors 103b (104b, 105b) (third angular velocity sensor) that detect the angular velocity around the axis parallel to the angular velocity sensors 103a (104a, 105a) (first angular velocity sensor) are also angular velocities. Similar to the sensors 103a (104a, 105a) (first angular velocity sensor), an example is shown in which the function of the primary side control circuit and the function of the secondary side control circuit can be interchanged. Not limited. In the present invention, the function of the primary side control circuit of the third angular velocity sensor and the function of the secondary side control circuit may be fixed (may not be replaced).
- a plurality of angular velocity sensors for detecting angular velocities around the three axes of the X-axis, the Y-axis, and the Z-axis that are orthogonal to each other are provided. Is not limited to this.
- a plurality of angular velocity sensors that detect angular velocities around two axes in different directions may be provided.
- a plurality of angular velocity sensors may be provided to detect the angular velocities around the four axes in different directions.
- the axes of the angular velocities detected by the plurality of angular velocity sensors may be in different directions that are not orthogonal to each other.
- the present invention is not limited to this.
- three or more angular velocity sensors for detecting angular velocities around parallel axes may be provided, a plurality of angular velocity sensors are provided for some of the axial velocities, and one angular velocity sensor is provided for other axial velocities. You may.
- Oscillator 11 Oscillator 12 Primary side control circuit 13 Secondary side control circuit 100 Azimuth angle attitude angle measuring device 101 Control unit 102 Power supply unit 103, 103a Angular velocity sensor (1st angular velocity sensor) 103b Angular velocity sensor (3rd angular velocity sensor) 104, 104a Angular velocity sensor (second angular velocity sensor) 105, 105a Angular velocity sensor (second angular velocity sensor)
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Abstract
Description
図1~図4を参照して、第1実施形態による方位角姿勢角計測装置100の構成について説明する。
第1実施形態では、以下のような効果を得ることができる。
次に、図5~図7を参照して、第2実施形態による方位角姿勢角計測装置200の構成について説明する。第2実施形態では、第1実施形態とは異なり、同軸の角速度を検出するために複数の角速度センサが設けられている構成の例について説明する。なお、第1実施形態と同様の構成については、同じ符号を付し、説明を省略する。
第2実施形態では、上記第1実施形態と同様に、角速度センサ103a、103b、104a、104b、105aおよび105bに、電源部102から安定して電力が供給されるので、演算に用いるための角速度を精度よく検出することができる。これにより、共通の電源部102に接続された複数の角速度センサ103a、103b、104a、104b、105aおよび105bの各々において、角速度を精度よく検出することができる。
なお、今回開示された実施形態は、すべての点で例示であって制限的なものではないと考えられるべきである。本発明の範囲は、上記した実施形態の説明ではなく請求の範囲によって示され、さらに請求の範囲と均等の意味および範囲内でのすべての変更が含まれる。
12 1次側制御回路
13 2次側制御回路
100 方位角姿勢角計測装置
101 制御部
102 電源部
103、103a 角速度センサ(第1角速度センサ)
103b 角速度センサ(第3角速度センサ)
104、104a 角速度センサ(第2角速度センサ)
105、105a 角速度センサ(第2角速度センサ)
Claims (12)
- 第1軸線回りの角速度を検出する第1角速度センサと、
前記第1軸線とは異なる方向の第2軸線回りの角速度を検出する第2角速度センサと、
前記第1角速度センサおよび前記第2角速度センサに電力を供給する電源部と、
制御部と、を備え、
前記第1角速度センサおよび前記第2角速度センサは、
振動子と、
閉じた制御ループを有し、前記閉じた制御ループの出力が前記振動子に1次振動を誘起させる1次側制御回路と、
前記振動子に印加される角速度に起因して前記振動子に発生する2次振動を検出する閉じた制御ループを有する2次側制御回路と、を各々含み、
前記1次側制御回路と前記2次側制御回路とは、前記1次側制御回路としての機能と、前記2次側制御回路としての機能とを入れ替え可能に構成されており、
前記制御部は、前記第1角速度センサおよび前記第2角速度センサのうちの一方において、前記1次側制御回路と前記2次側制御回路との機能を入れ替える前後で演算に用いるための角速度を検出している場合に、前記第1角速度センサおよび前記第2角速度センサのうちの他方において、前記1次側制御回路と前記2次側制御回路との機能を入れ替える制御を行わないように構成されている、方位角姿勢角計測装置。 - 前記制御部は、前記2次側制御回路により前記振動子の2次振動を検出した角速度の検出結果と、前記1次側制御回路と前記2次側制御回路との機能を入れ替えて、前記1次側制御回路により前記振動子の2次振動を検出した角速度の検出結果と、に基づいて、前記第1角速度センサおよび前記第2角速度センサにより検出する角速度のバイアス成分をキャンセルする演算を行うように構成されている、請求項1に記載の方位角姿勢角計測装置。
- 前記制御部は、前記1次側制御回路と前記2次側制御回路との機能を入れ替える前後の所定期間は、角速度のバイアス成分をキャンセルするための角速度の検出を中断するように構成されている、請求項2に記載の方位角姿勢角計測装置。
- 前記制御部は、前記第1角速度センサおよび前記第2角速度センサのうちの一方における、前記1次側制御回路と前記2次側制御回路との機能を入れ替える前後の所定期間において、前記第1角速度センサおよび前記第2角速度センサのうちの他方における、前記1次側制御回路と前記2次側制御回路との機能を入れ替える制御を行うように構成されている、請求項1に記載の方位角姿勢角計測装置。
- 前記制御部は、前記第1角速度センサおよび前記第2角速度センサにおける、前記1次側制御回路と前記2次側制御回路との機能を入れ替えるタイミングを略同時にするように構成されている、請求項4に記載の方位角姿勢角計測装置。
- 振動子を含み、前記第1軸線回りの角速度を検出する第3角速度センサをさらに備え、
前記電源部は、前記第1角速度センサおよび前記第2角速度センサに加えて、前記第3角速度センサに電力を供給するように構成されており、
前記制御部は、前記第3角速度センサにおいて、演算に用いるための角速度を検出している場合に、前記第1角速度センサにおいて、前記1次側制御回路と前記2次側制御回路との機能を入れ替える制御を行わないように構成されている、請求項1に記載の方位角姿勢角計測装置。 - 第1軸線回りの角速度を検出する第1角速度センサと、
前記第1軸線とは異なる方向の第2軸線回りの角速度を検出する第2角速度センサと、
前記第1角速度センサおよび前記第2角速度センサに電力を供給する電源部と、
制御部と、を備え、
前記第1角速度センサおよび前記第2角速度センサは、
振動子と、
閉じた制御ループを有し、前記閉じた制御ループの出力が前記振動子に1次振動を誘起させる1次側制御回路と、
前記振動子に印加される角速度に起因して前記振動子に発生する2次振動を検出する閉じた制御ループを有する2次側制御回路と、を各々含み、
前記1次振動を誘起する機能と前記2次振動を検出する機能とを入れ替え可能に構成されており、
前記制御部は、前記第1角速度センサおよび前記第2角速度センサのうちの一方において、前記1次振動を誘起する機能と前記2次振動を検出する機能とを入れ替える前後で演算に用いるための角速度を検出している場合に、前記第1角速度センサおよび前記第2角速度センサのうちの他方において、前記1次振動を誘起する機能と前記2次振動を検出する機能とを入れ替える制御を行わないように構成されている、方位角姿勢角計測装置。 - 前記制御部は、前記振動子の前記2次振動を検出した角速度の検出結果と、前記1次振動を誘起する機能と前記2次振動を検出する機能とを入れ替えて前記振動子の前記2次振動を検出した角速度の検出結果と、に基づいて、前記第1角速度センサおよび前記第2角速度センサにより検出する角速度のバイアス成分をキャンセルする演算を行うように構成されている、請求項7に記載の方位角姿勢角計測装置。
- 前記制御部は、前記1次振動を誘起する機能と前記2次振動を検出する機能とを入れ替える前後の所定期間は、角速度のバイアス成分をキャンセルするための角速度の検出を中断するように構成されている、請求項8に記載の方位角姿勢角計測装置。
- 前記制御部は、前記第1角速度センサおよび前記第2角速度センサのうちの一方における、前記1次振動を誘起する機能と前記2次振動を検出する機能とを入れ替える前後の所定期間において、前記第1角速度センサおよび前記第2角速度センサのうちの他方における、前記1次振動を誘起する機能と前記2次振動を検出する機能とを入れ替える制御を行うように構成されている、請求項7に記載の方位角姿勢角計測装置。
- 前記制御部は、前記第1角速度センサおよび前記第2角速度センサにおける、前記1次振動を誘起する機能と前記2次振動を検出する機能とを入れ替えるタイミングを略同時にするように構成されている、請求項10に記載の方位角姿勢角計測装置。
- 振動子を含み、前記第1軸線回りの角速度を検出する第3角速度センサをさらに備え、
前記電源部は、前記第1角速度センサおよび前記第2角速度センサに加えて、前記第3角速度センサに電力を供給するように構成されており、
前記制御部は、前記第3角速度センサにおいて、演算に用いるための角速度を検出している場合に、前記第1角速度センサにおいて、前記1次振動を誘起する機能と前記2次振動を検出する機能とを入れ替える制御を行わないように構成されている、請求項7に記載の方位角姿勢角計測装置。
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CA3175876A CA3175876A1 (en) | 2020-03-24 | 2021-03-23 | Azimuth/attitude angle measuring device |
EP21776668.2A EP4130662A4 (en) | 2020-03-24 | 2021-03-23 | AZIMUTH/ANGLE MEASURING DEVICE |
US17/913,251 US20230140455A1 (en) | 2020-03-24 | 2021-03-23 | Azimuth/Attitude Angle Measuring Device |
AU2021243388A AU2021243388B2 (en) | 2020-03-24 | 2021-03-23 | Azimuth/attitude angle measuring device |
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JP2007520716A (ja) * | 2004-02-04 | 2007-07-26 | ビ−エイイ− システムズ パブリック リミテッド カンパニ− | 振動構造ジャイロスコープにおけるバイアス誤差を低減する方法 |
JP2009115559A (ja) | 2007-11-05 | 2009-05-28 | Sumitomo Precision Prod Co Ltd | 角速度センサ及び角速度センサを備えた電子機器 |
CN108253952A (zh) * | 2017-12-01 | 2018-07-06 | 北京时代民芯科技有限公司 | 一种零偏自校准mems陀螺仪及其零偏自校准方法 |
JP2018151200A (ja) * | 2017-03-10 | 2018-09-27 | 住友精密工業株式会社 | 振動型角速度センサ |
JP6761140B1 (ja) * | 2020-03-24 | 2020-09-23 | 住友精密工業株式会社 | 振動型角速度センサ |
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WO2001079862A1 (en) | 2000-04-14 | 2001-10-25 | Microsensors, Inc. | Z-axis micro-gyro |
JP2004053530A (ja) * | 2002-07-23 | 2004-02-19 | National Institute Of Advanced Industrial & Technology | 移動体の高精度姿勢検出方法及びその装置 |
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JP2007520716A (ja) * | 2004-02-04 | 2007-07-26 | ビ−エイイ− システムズ パブリック リミテッド カンパニ− | 振動構造ジャイロスコープにおけるバイアス誤差を低減する方法 |
JP2009115559A (ja) | 2007-11-05 | 2009-05-28 | Sumitomo Precision Prod Co Ltd | 角速度センサ及び角速度センサを備えた電子機器 |
JP2018151200A (ja) * | 2017-03-10 | 2018-09-27 | 住友精密工業株式会社 | 振動型角速度センサ |
CN108253952A (zh) * | 2017-12-01 | 2018-07-06 | 北京时代民芯科技有限公司 | 一种零偏自校准mems陀螺仪及其零偏自校准方法 |
JP6761140B1 (ja) * | 2020-03-24 | 2020-09-23 | 住友精密工業株式会社 | 振動型角速度センサ |
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US20230140455A1 (en) | 2023-05-04 |
AU2021243388B2 (en) | 2024-03-07 |
CA3175876A1 (en) | 2021-09-30 |
AU2021243388A1 (en) | 2022-11-10 |
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