CN111856355B - System and method for keeping optimal sensitivity of magnetometer - Google Patents
System and method for keeping optimal sensitivity of magnetometer Download PDFInfo
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- CN111856355B CN111856355B CN202010688276.9A CN202010688276A CN111856355B CN 111856355 B CN111856355 B CN 111856355B CN 202010688276 A CN202010688276 A CN 202010688276A CN 111856355 B CN111856355 B CN 111856355B
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- G01—MEASURING; TESTING
- G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
- G01R33/00—Arrangements or instruments for measuring magnetic variables
- G01R33/02—Measuring direction or magnitude of magnetic fields or magnetic flux
- G01R33/06—Measuring direction or magnitude of magnetic fields or magnetic flux using galvano-magnetic devices
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- G01R33/096—Magnetoresistive devices anisotropic magnetoresistance sensors
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- G—PHYSICS
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- G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
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- G01R33/0035—Calibration of single magnetic sensors, e.g. integrated calibration
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Abstract
The invention relates to a system and a method for keeping the optimal sensitivity of a magnetometer, which can be used for automatically calibrating in real time and keeping the optimal sensitivity of the magnetometer and are suitable for application occasions where the satellite-borne magnetometer is continuously tested for a long time and manual calibration cannot be carried out. By adding the oblique S magnetic sensors, under different judgment thresholds of the residual error module, data processing, setting and resetting operations are performed on the three orthogonal magnetic sensors, so that the system can keep optimal sensitivity in real time, the setting and resetting operations of the three orthogonal magnetic sensors are obviously reduced, and the power consumption of the system is greatly reduced. The invention can obviously keep the accuracy and the optimal sensitivity of system measurement, and simultaneously reduces the power consumption of the system and improves the reliability of the system and the like by reducing the times of setting and resetting operations of the system.
Description
Technical Field
The invention relates to a system and a method for keeping the optimal sensitivity of a magnetometer, which can be used for automatically calibrating in real time and keeping the optimal sensitivity of the magnetometer and are suitable for application occasions where the satellite-borne magnetometer is continuously tested for a long time and manual calibration cannot be carried out.
Background
A magnetometer based on the anisotropic magneto-resistance effect (AMR) has the advantages of high sensitivity, small volume, convenience in installation and the like, can be used for assisting in measuring the change of the attitude of a low-orbit microsatellite, and is generally composed of three orthogonally-configured AMR magnetic sensors. The basic structure of the AMR magnetic sensor is a Wheatstone bridge consisting of four magnetic resistances, when an external bias magnetic field is applied to the bridge, the magnetization directions of two oppositely-arranged resistors rotate towards the current direction, and the resistance values of the two corresponding resistors are increased; and the resistance values of the other two oppositely-arranged resistors can be reduced, and the external magnetic field value can be obtained by measuring the differential pressure signals of the two output ends of the bridge.
A magnetometer based on an AMR magnetic sensor measures the change of the attitude of a satellite by measuring the change of the included angle between the microsatellite and the earth magnetic field of the orbit, and usually needs to continuously work in the orbit for months or years. With long-time power-up work, the initial magnetic domain polarization direction in the AMR magnetic sensor can deflect, so that additional bias is brought to the measurement of a magnetic field, the accuracy of the magnetic field measurement is influenced, the magnetic domain polarization strength can decline, and the measurement sensitivity of a magnetometer is reduced. When the magnetometer is applied to low-orbit satellite attitude measurement, the magnetometer is also subjected to special environment interference such as space radiation, and the like, so that the measurement sensitivity of the magnetometer is reduced. In addition, the geomagnetic field at the low orbit becomes weaker relative to the earth's surface, and the magnetometer is also required to maintain optimal sensitivity in real time in order to ensure accurate measurement of the satellite attitude.
When the magnetometer is applied to the measurement of the earth surface geomagnetic field, the optimal sensitivity of the magnetometer can be kept by utilizing external calibration equipment and adopting a manual calibration mode. When the magnetometer is applied to geomagnetic measurement of a space orbit for a long time, the optimal sensitivity of the magnetometer cannot be ensured in a manual calibration mode.
The traditional magnetometer carries out setting and resetting operations on a magnetic sensor in real time before the acquisition of measurement data. Although this method can maintain the sensitivity of the magnetometer measurement, it requires a large pulse current for the set and reset operations, which results in large power consumption of the system.
Disclosure of Invention
The technical problem to be solved by the invention is as follows: the defects of the prior art are overcome, and a system and a method for keeping the optimal sensitivity of the magnetometer are provided: the system and the method are characterized in that an inclined magnetic sensor is added and keeps a certain included angle with other three orthogonally arranged magnetic sensors, the inclined magnetic sensor carries out residual error estimation under the assistance of a setting module and a resetting module, and then the operation processing is carried out on the other three orthogonally arranged magnetic sensors. The invention is simple and reliable, does not need manual calibration, obviously reduces the system power consumption, and improves the accuracy and the reliability of the measurement of the magnetometer.
The purpose of the invention is realized by the following technical scheme:
a system for keeping the optimal sensitivity of a magnetometer comprises an S magnetic sensor, an X magnetic sensor, a Y magnetic sensor, a Z magnetic sensor, a setting and resetting module, a residual error estimation module, a switch 1 module, a switch 2 module and an output control module;
the X magnetic sensor, the Y magnetic sensor and the Z magnetic sensor are installed in a mutually orthogonal mode in pairs;
the S magnetic sensor is obliquely arranged, the fixed included angle between the S magnetic sensor and the X magnetic sensor is alpha, the fixed included angle between the S magnetic sensor and the Y magnetic sensor is beta, and the fixed included angle between the S magnetic sensor and the Z magnetic sensor is gamma; wherein, the alpha, the beta and the gamma are not equal in pairs;
the setting and resetting module is used for carrying out setting and resetting operations on the S magnetic sensor at a set period, and is also used for carrying out setting and resetting operations on the X magnetic sensor, the Y magnetic sensor and the Z magnetic sensor simultaneously when the switch 2 module is in an open state;
the S magnetic sensor is used for outputting the set output signal S + And is also used for outputting the reset output signal S - And generating an output signal S + And an output signal S - Outputting the residual error to a residual error estimation module; when the switch 1 module is in the on state, the S magnetic sensor is also used for outputting a signal S - Output to the output control module;
the residual error estimation module is used for receiving the output signal S + And output signal S - And to the received output signal S + And output signal S - After residual error processing is carried out, a judgment threshold value P1 is output to a switch 1 module, and a judgment threshold value P2 is output to a switch 2 module; when the judgment threshold value P1 is 1, the switch 1 module is started, when the judgment threshold value P1 is not 1, the switch 1 module is in a closed state, when the judgment threshold value P2 is 1, the switch 2 module is started, and when the judgment threshold value P2 is not 1, the switch 2 module is in a closed state;
the output control module is used for receiving an output signal S output by the S magnetic sensor when the switch 1 module is in an open state - The output control module is also used for receiving the output signal S of the X magnetic sensor x Output signal S of the Y magnetic sensor y And the output signal S of the Z magnetic sensor z When the switch 1 module is in the on state, the output control module processes the received signal to generate the corrected S x ' Signal, S y ' Signal and S z ' signals are used for three-axis control of the satellite;
the setting and resetting module carries out setting and resetting operations on the polarization resistance band of the S magnetic sensor in real time, and a complete operation cycle is f 0 =48kHz, in which the set and reset operations are both continued for:
the residual error processing process comprises the following steps:
firstly, the residual error estimation module sets the output signal S of the S magnetic sensor + The treatment comprises the following steps:
secondly, the residual error estimation module outputs the output signal S of the magnetic sensor S after reset - The treatment comprises the following steps:
thirdly, the residual error estimation module performs the following data processing according to the formula (2) and the formula (3):
and fourthly, the residual error estimation module judges according to the formula (4) and gives out a judgment threshold value:
that is, the residual estimation module sets the values of the judgment thresholds P1 and P2 according to the equations (2) - (5), where Y is 0 Is a preset constant residual error value;
when the switch 1 module is in an on state, the method for the output control module to process the received signal comprises the following steps:
a method of maintaining optimal sensitivity of a magnetometer, comprising the steps of:
(1) The S magnetic sensor is set and reset by the set and reset module in a set period;
(2) The S magnetic sensor generates a set output signal S under the action of the setting and resetting module + And the output signal S after reset - And then S is + And S - The signal is output to a residual error estimation module;
(3) Residual estimation module for received output signal S + And output signal S - Residual error processing is carried out, an output judgment threshold value P1 is obtained through calculation and is output to a switch 1 module, an output judgment threshold value P2 is obtained through calculation and is output to a switch 2 module;
(4) When the judgment threshold P1 is 1, the switch 1 module is started, when the judgment threshold P1 is not 1, the switch 1 module is closed, when the judgment threshold P2 is 1, the switch 2 module is started, and when the judgment threshold P2 is not 1, the switch 2 module is closed;
(5) When the switch 1 module is turned on, the output control module receives the output signal S output by the S magnetic sensor - Output signal S of, X magnetic sensor x Output signal S of the Y magnetic sensor y And the output signal S of the Z magnetic sensor z Processing to generate corrected S x ' Signal, S y ' Signal and S z ' signals are used for three-axis control of the satellite;
(6) When the switch 2 module is turned on, the set and reset module simultaneously sets and resets the X magnetic sensor, the Y magnetic sensor, and the Z magnetic sensor.
Compared with the prior art, the invention has the following beneficial effects:
(1) The invention adds the S magnetic sensor, carries out residual estimation in real time, and controls and operates other three magnetic sensors according to the estimated judgment threshold value.
(2) The S magnetic sensor performs setting and resetting operations in real time, and the output control module performs output operation processing on the S magnetic sensor and the X magnetic sensor, the Y magnetic sensor and the Z magnetic sensor, so that magnetic field measurement of the X magnetic sensor, the Y magnetic sensor and the Z magnetic sensor is more accurate.
(3) The invention reduces the setting and resetting operation times of the X magnetic sensor, the Y magnetic sensor and the Z magnetic sensor in the long-term use process, namely reduces the use of large current pulses and obviously reduces the power consumption of the system.
(4) Setting operation is realized by applying a normal-phase large current with the amplitude of 4 amperes and the width of 50 nanoseconds to the polarization resistance band of the S magnetic sensor, and the output signal of the S magnetic sensor is recorded as S + (ii) a The reset operation is realized by applying a large negative-phase current with the amplitude of 4 amperes and the width of 50 nanoseconds to the polarized resistance band of the S magnetic sensor, and the output signal of the S magnetic sensor is recorded as S - (ii) a The polarization resistance bands of the X magnetic sensor, the Y magnetic sensor, and the Z magnetic sensor are connected in series; setting operations of the X magnetic sensor, the Y magnetic sensor and the Z magnetic sensor are realized by applying normal-phase large current with the amplitude of 4 amperes and the width of 50 nanoseconds; the reset operation of the X magnetic sensor, the Y magnetic sensor and the Z magnetic sensor is realized by implementing a negative phase large current with the amplitude of 4 amperes and the width of 50 nanoseconds;
(5) According to the system and the method for maintaining the optimal sensitivity of the magnetometer, provided by the invention, the data processing and the setting and resetting operations are carried out on the three orthogonal magnetic sensors under different judgment thresholds of the residual error module by adding the obliquely-arranged S magnetic sensors, so that the system can maintain the optimal sensitivity in real time, the setting and resetting operations of the three orthogonal magnetic sensors are obviously reduced, and the power consumption of the system is greatly reduced. The invention can obviously keep the accuracy and the optimal sensitivity of system measurement, and simultaneously reduces the power consumption of the system and improves the reliability of the system and the like by reducing the times of setting and resetting operations of the system.
Drawings
FIG. 1 is a schematic view of the mounting configuration of an S-magnetic sensor and a tri-orthogonal magnetic sensor of the present invention;
FIG. 2 is a block diagram of the system of the present invention;
fig. 3 is a schematic diagram of a series connection mode of polarization resistance bands of the three orthogonal magnetic sensors.
Detailed Description
To make the objects, technical solutions and advantages of the present invention more apparent, embodiments of the present invention will be described in further detail below with reference to the accompanying drawings.
A system for maintaining optimal sensitivity of a magnetometer comprises the following specific embodiments:
as shown in fig. 2, the magnetic sensor includes an S magnetic sensor 1, a set/reset module 6, a residual estimation module 5, a switch 1 module 7, a switch 2 module 8, and an output control module 9.
The four magnetic sensors of the inventive system are mounted in the configuration shown in fig. 1: the X magnetic sensor 2, the Y magnetic sensor 3 and the Z magnetic sensor 4 are installed in a mutually orthogonal mode in pairs; the S magnetic sensor 1 is obliquely installed, and installation included angles between the S magnetic sensor 1 and the X magnetic sensor 2, between the Y magnetic sensor 3 and between the S magnetic sensor 4 and the Z magnetic sensor are respectively alpha, beta and gamma, wherein the alpha, the beta and the gamma are not equal to each other in pairs.
The X magnetic sensor 2, the Y magnetic sensor 3 and the Z magnetic sensor 4 are mainly used for completing the deflection angle postures of the satellite along the X axis, the Y axis and the Z axis; the S magnetic sensor 1 is used to assist and control the X magnetic sensor 2, the Y magnetic sensor 3, and the Z magnetic sensor 4 by the residual estimation module 5.
A method for maintaining optimal sensitivity of a magnetometer comprises the following specific implementation modes:
the setting and resetting module 6 sets and resets the polarization resistance band of the S magnetic sensor 1 in real time. One complete operation cycle is f 0 =48kHz, where the set and reset operations each last approximately:
setting operation is realized by applying normal-phase large current with the amplitude of 4 amperes and the width of 50 nanoseconds to the polarized resistance strip of the S magnetic sensor, and the output signal of the S magnetic sensor is recorded as S + (ii) a The reset operation was performed by applying a polarized resistance band of the S-magnetic sensor with an amplitude of 4 amperes and a width of 50 nanosecondsThe negative phase is realized by large current, and the output signal of the S magnetic sensor is recorded as S - ;
The residual estimation module 5 performs residual estimation according to the output signal of the set and reset S magnetic sensor, and provides a judgment threshold, and the specific method is as follows:
the residual estimation module 5 firstly sets the output signal S of the S magnetic sensor + The treatment comprises the following steps:
the residual estimation module 5 first outputs the reset S output signal S of the magnetic sensor - The treatment comprises the following steps:
then, the residual estimation module 5 performs the following data processing according to equations (2) and (3):
finally, the residual estimation module 5 performs judgment according to equation (4), and gives a judgment threshold:
that is, the residual block 5 sets the values of the judgment thresholds P1 and P2 according to the equations (2) to (5), where Y is 0 Is a preset constant residual error value;
when the determination threshold P1 is 1, the switch 1 module 7 is turned on, and at this time, the output control module 9 performs output operation processing of the S magnetic sensor 1 and the X magnetic sensor 2, the Y magnetic sensor 3, and the Z magnetic sensor 4, specifically:
wherein S is x 、S x And S z Raw outputs of the X magnetic sensor 2, the Y magnetic sensor 3, and the Z magnetic sensor 4, respectively; s x '、S y ' and S z ' is the final Z-axis, Y-axis and Z-axis measurement output of the system magnetometer.
When the determination threshold P2 is 1, the switch 2 module 8 is turned on, and the set/reset module 6 sets and resets the X magnetic sensor 2, the Y magnetic sensor 3, and the Z magnetic sensor 4. The polarization resistance bands of the X magnetic sensor 2, the Y magnetic sensor 3, and the Z magnetic sensor 4 are connected in series as shown in fig. 3. Setting operations of the X magnetic sensor 2, the Y magnetic sensor 3 and the Z magnetic sensor 4 are realized by implementing normal-phase large current with the amplitude of 4 amperes and the width of 50 nanoseconds; the reset operation of the X magnetic sensor 2, the Y magnetic sensor 3 and the Z magnetic sensor 4 is realized by implementing a negative phase large current with the amplitude of 4 amperes and the width of 50 nanoseconds;
in summary, the system and the method for maintaining the optimal sensitivity of the magnetometer provided by the invention perform data processing and setting and resetting operations on three orthogonal magnetic sensors under different judgment thresholds of the residual error module by adding the obliquely-arranged S magnetic sensors, so that the system can maintain the optimal sensitivity in real time, and meanwhile, the setting and resetting operations of the three orthogonal magnetic sensors are significantly reduced, and the power consumption of the system is greatly reduced.
Those skilled in the art will appreciate that those matters not described in detail in the present specification are well known in the art.
Claims (9)
1. A system for maintaining optimal sensitivity of a magnetometer, comprising: the system comprises an S magnetic sensor, an X magnetic sensor, a Y magnetic sensor, a Z magnetic sensor, a setting and resetting module, a residual error estimation module, a switch 1 module, a switch 2 module and an output control module;
the X magnetic sensor, the Y magnetic sensor and the Z magnetic sensor are installed in a mutually orthogonal mode in pairs;
the S magnetic sensor is obliquely arranged, the fixed included angle between the S magnetic sensor and the X magnetic sensor is alpha, the fixed included angle between the S magnetic sensor and the Y magnetic sensor is beta, and the fixed included angle between the S magnetic sensor and the Z magnetic sensor is gamma; wherein, the alpha, the beta and the gamma are not equal in pairs;
the setting and resetting module is used for carrying out setting and resetting operations on the S magnetic sensor in a set period, and is also used for carrying out setting and resetting operations on the X magnetic sensor, the Y magnetic sensor and the Z magnetic sensor simultaneously when the switch 2 module is in an on state;
the S magnetic sensor is used for outputting the set output signal S + And is also used for outputting the reset output signal S - And will generate an output signal S + And an output signal S - Outputting the residual error to a residual error estimation module; when the switch 1 module is in the on state, the S magnetic sensor is also used for outputting a signal S - Output to the output control module;
the residual error estimation module is used for receiving the output signal S + And output signal S - And to the received output signal S + And output signal S - After residual error processing is carried out, a judgment threshold value P1 is output to a switch 1 module, and a judgment threshold value P2 is output to a switch 2 module; when the judgment threshold value P1 is 1, the switch 1 module is started, when the judgment threshold value P1 is not 1, the switch 1 module is in a closed state, when the judgment threshold value P2 is 1, the switch 2 module is started, and when the judgment threshold value P2 is not 1, the switch 2 module is in a closed state;
the residual error processing process comprises the following steps:
firstly, the residual error estimation module sets the output signal S of the S magnetic sensor + The treatment comprises the following steps:
secondly, the residual error estimation module outputs the output signal S of the S magnetic sensor after reset - The treatment comprises the following steps:
thirdly, the residual estimation module performs the following data processing according to the formula (2) and the formula (3):
and fourthly, the residual error estimation module judges according to the formula (4) and gives out a judgment threshold value:
wherein Y is 0 Is a preset constant residual error value;
the output control module is used for receiving an output signal S output by the S magnetic sensor when the switch 1 module is in an open state - The output control module is also used for receiving the output signal S of the X magnetic sensor x Output signal S of the Y magnetic sensor y And the output signal S of the Z magnetic sensor z When the switch 1 module is in the on state, the output control module processes the received signal to generate the corrected S x ' Signal, S y ' Signal and S z ' the signal is used for three-axis control of the satellite.
2. A system for maintaining optimal sensitivity of a magnetometer according to claim 1 wherein: the setting and resetting module carries out setting and resetting operations on the polarized resistance band of the S magnetic sensor in real time, and a complete operation cycle is f 0 =48kHz。
5. a system for maintaining optimal sensitivity of a magnetometer according to claim 1 wherein: the polarization resistance bands of the X magnetic sensor, the Y magnetic sensor, and the Z magnetic sensor are connected in series.
6. A system for maintaining optimal sensitivity of a magnetometer according to claim 1 wherein: the set operation was performed by applying a positive phase current of 4 amperes and 50 nanoseconds in width to the polarization resistance band of the S-magnetic sensor.
7. A system for maintaining optimal sensitivity of a magnetometer according to claim 1 wherein: the reset operation is realized by applying a negative phase current having an amplitude of 4 amperes and a width of 50 nanoseconds to the polarization resistance band of the S-magnetic sensor.
8. A method of maintaining optimal sensitivity of a magnetometer according to claim 1 wherein the steps comprise:
(1) The S magnetic sensor is set and reset by the set and reset module in a set period;
(2) The S magnetic sensor generates a set output signal S under the action of the setting and resetting module + And the output signal S after reset - And then S is + And S - The signal is output to a residual error estimation module;
(3) Residual estimation module receives output signal S + And output signal S - To carry outResidual error processing, namely calculating to obtain an output judgment threshold value P1, outputting the output judgment threshold value P1 to a switch 1 module, calculating to obtain an output judgment threshold value P2, and outputting the output judgment threshold value P2 to a switch 2 module;
(4) When the judgment threshold value P1 is 1, the switch 1 module is turned on, when the judgment threshold value P1 is not 1, the switch 1 module is turned off, when the judgment threshold value P2 is 1, the switch 2 module is turned on, and when the judgment threshold value P2 is not 1, the switch 2 module is turned off;
(5) When the switch 1 module is turned on, the output control module receives the output signal S output by the S magnetic sensor - Output signal S of, X magnetic sensor x And an output signal S of the Y magnetic sensor y And the output signal S of the Z magnetic sensor z Processing to generate corrected S x ' Signal, S y ' Signal sum S z ' the signal is used for three-axis control of the satellite.
9. A method of maintaining optimal sensitivity of a magnetometer according to claim 8 wherein: when the switch 2 module is turned on, the set and reset module simultaneously sets and resets the X magnetic sensor, the Y magnetic sensor, and the Z magnetic sensor.
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Citations (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2003014460A (en) * | 2001-06-29 | 2003-01-15 | Japan Aviation Electronics Industry Ltd | Attitude angle detector |
WO2011158856A1 (en) * | 2010-06-17 | 2011-12-22 | 株式会社フジクラ | Error cause determination method and device, error compensation method, three-axis magnetic sensor, sensor module, and program for determining error cause |
CN104614689A (en) * | 2015-01-22 | 2015-05-13 | 北京航空航天大学 | Giant magneto-impedance effect-based magnetic field gradient sensor |
CN104898075A (en) * | 2015-06-18 | 2015-09-09 | 哈尔滨工程大学 | High-precision relative magnetic field intensity measuring device |
CN105005010A (en) * | 2015-07-06 | 2015-10-28 | 电子科技大学 | Low-power magnetic resistance sensor based on LTCC technology and preparation method therefor |
CN105022005A (en) * | 2014-04-23 | 2015-11-04 | 中国科学院上海微系统与信息技术研究所 | SQUID magnetic sensor measuring sensitivity enhancement method, device and system |
CN204789958U (en) * | 2015-05-06 | 2015-11-18 | 广州番禺职业技术学院 | Magneto resistive sensor operating circuit |
CN105487026A (en) * | 2016-01-26 | 2016-04-13 | 东北电力大学 | Three-axis magnetic field intensity meter based on giant magnetoresistance effect chip |
CN105676303A (en) * | 2016-01-19 | 2016-06-15 | 南京理工大学 | Terrestrial magnetism data collector |
CN205809273U (en) * | 2016-04-06 | 2016-12-14 | 江苏多维科技有限公司 | A kind of anisotropic magnetoresistance AMR sensor without set/reset device |
CN207020294U (en) * | 2017-05-26 | 2018-02-16 | 陕西瑞特测控技术有限公司 | A kind of three-axle magnetic field meter based on magnetoresistive transducer |
WO2019020945A1 (en) * | 2017-07-26 | 2019-01-31 | Sysnav | Method for calibrating a magnetometer |
CN109932672A (en) * | 2019-03-27 | 2019-06-25 | 上海微小卫星工程中心 | A method of the error of amendment three axis magnetometer |
CN110030991A (en) * | 2019-04-04 | 2019-07-19 | 湖南国科赢纳科技有限公司 | Merge the flying object high speed rotation angular movement measurement method of gyro and magnetometer |
CN110118948A (en) * | 2019-06-04 | 2019-08-13 | 中国科学院上海微系统与信息技术研究所 | A kind of the resultant field measurement method and device of based superconductive quantum inteferometer |
CN110515023A (en) * | 2019-10-11 | 2019-11-29 | 深圳航天东方红海特卫星有限公司 | A kind of microsatellite three axis magnetometer bearing calibration |
WO2020005580A1 (en) * | 2018-06-25 | 2020-01-02 | Gatekeeper Systems, Inc. | Dual magnetometer calibration |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7057173B2 (en) * | 2004-01-05 | 2006-06-06 | Laser Technology, Inc. | Magnetoresistive (MR) sensor temperature compensation and magnetic cross-term reduction techniques utilizing selective set and reset gain measurements |
US8525514B2 (en) * | 2010-03-19 | 2013-09-03 | Memsic, Inc. | Magnetometer |
-
2020
- 2020-07-16 CN CN202010688276.9A patent/CN111856355B/en active Active
Patent Citations (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2003014460A (en) * | 2001-06-29 | 2003-01-15 | Japan Aviation Electronics Industry Ltd | Attitude angle detector |
WO2011158856A1 (en) * | 2010-06-17 | 2011-12-22 | 株式会社フジクラ | Error cause determination method and device, error compensation method, three-axis magnetic sensor, sensor module, and program for determining error cause |
CN105022005A (en) * | 2014-04-23 | 2015-11-04 | 中国科学院上海微系统与信息技术研究所 | SQUID magnetic sensor measuring sensitivity enhancement method, device and system |
CN104614689A (en) * | 2015-01-22 | 2015-05-13 | 北京航空航天大学 | Giant magneto-impedance effect-based magnetic field gradient sensor |
CN204789958U (en) * | 2015-05-06 | 2015-11-18 | 广州番禺职业技术学院 | Magneto resistive sensor operating circuit |
CN104898075A (en) * | 2015-06-18 | 2015-09-09 | 哈尔滨工程大学 | High-precision relative magnetic field intensity measuring device |
CN105005010A (en) * | 2015-07-06 | 2015-10-28 | 电子科技大学 | Low-power magnetic resistance sensor based on LTCC technology and preparation method therefor |
CN105676303A (en) * | 2016-01-19 | 2016-06-15 | 南京理工大学 | Terrestrial magnetism data collector |
CN105487026A (en) * | 2016-01-26 | 2016-04-13 | 东北电力大学 | Three-axis magnetic field intensity meter based on giant magnetoresistance effect chip |
CN205809273U (en) * | 2016-04-06 | 2016-12-14 | 江苏多维科技有限公司 | A kind of anisotropic magnetoresistance AMR sensor without set/reset device |
CN207020294U (en) * | 2017-05-26 | 2018-02-16 | 陕西瑞特测控技术有限公司 | A kind of three-axle magnetic field meter based on magnetoresistive transducer |
WO2019020945A1 (en) * | 2017-07-26 | 2019-01-31 | Sysnav | Method for calibrating a magnetometer |
WO2020005580A1 (en) * | 2018-06-25 | 2020-01-02 | Gatekeeper Systems, Inc. | Dual magnetometer calibration |
CN109932672A (en) * | 2019-03-27 | 2019-06-25 | 上海微小卫星工程中心 | A method of the error of amendment three axis magnetometer |
CN110030991A (en) * | 2019-04-04 | 2019-07-19 | 湖南国科赢纳科技有限公司 | Merge the flying object high speed rotation angular movement measurement method of gyro and magnetometer |
CN110118948A (en) * | 2019-06-04 | 2019-08-13 | 中国科学院上海微系统与信息技术研究所 | A kind of the resultant field measurement method and device of based superconductive quantum inteferometer |
CN110515023A (en) * | 2019-10-11 | 2019-11-29 | 深圳航天东方红海特卫星有限公司 | A kind of microsatellite three axis magnetometer bearing calibration |
Non-Patent Citations (6)
Title |
---|
《3-D 磁传感器的电路设计与信号处理》;郭家玉等;《自动化与仪表》;20081231;5-9 * |
《三轴磁敏传感器误差分析与校正研究》;李久春;《测控技术》;20081231;11-13 * |
《地磁信号检测系统误差分析与补偿方法研究》;黄学功等;《兵工学报》;20110131;第32卷(第1期);33-36 * |
《基于磁阻传感器的姿态测量系统研究》;张晓肖;《中国优秀硕士学位论文全文数据库 (信息科技辑)》;20200228;14-18 * |
《应用于皮卫星的地球磁场测量系统设计》;蔡波第;《传 感 技 术 学 报》;20110831;1212-1216 * |
《用于组合导航系统的三轴地磁导航传感器设计》;金海红等;《无线互联科技》;20200331;85-88 * |
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