CN103472259A - Method for silicon micro-resonant type accelerometer temperature compensation - Google Patents
Method for silicon micro-resonant type accelerometer temperature compensation Download PDFInfo
- Publication number
- CN103472259A CN103472259A CN2013104297031A CN201310429703A CN103472259A CN 103472259 A CN103472259 A CN 103472259A CN 2013104297031 A CN2013104297031 A CN 2013104297031A CN 201310429703 A CN201310429703 A CN 201310429703A CN 103472259 A CN103472259 A CN 103472259A
- Authority
- CN
- China
- Prior art keywords
- resonance
- voltage
- driving
- temperature
- frequency
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Images
Abstract
The invention discloses a method for silicon micro-resonant type accelerometer temperature compensation. The method comprises the steps that firstly, under the condition that the accelerated speed does not exist, a singular change relation curve of a direct current drive voltage maintaining the constant resonant amplitude of a resonant beam and the resonant frequency of the resonant beam is calibrated; secondly, under the condition that the accelerated speed exists, the direct current drive voltage and the resonant frequency are measured; thirdly, combined with the previously obtained relation curve, the resonant frequency caused by the temperature is subtracted from the resonant frequency obtained through measurement and the temperature compensation operation is completed. According to the method for silicon micro-resonant type accelerometer temperature compensation, the defect that large deviation of a compensation result is caused by the non-determinacy of temperature field distribution in a traditional direct temperature compensation method and heat conduction delay is overcome, and real-time and high-accuracy temperature compensation is achieved. According to the method, the cost of temperature compensation is low, sensors do not need to be additionally arranged, and temperature compensation can be achieved through existing circuit devices.
Description
Technical field
The present invention relates to a kind of silicon micro-resonance type accelerometer temperature compensation, relate in particular to and a kind ofly utilize accelerometer self drive voltage signal but not directly measure temperature signal and silicon micro-resonance type accelerometer is carried out to the method for temperature compensation.
Background technology
Silicon micro-resonance type accelerometer is based on MEMS technique, and two resonance beam that are forced to flexural vibrations of take are the power sensing unit, the poor size that characterizes suffered acceleration of vibration frequency of two resonance beam (resonance beam 1 and resonance beam 2).Because the elastic modulus temperature influence of resonance beam, and the silicon micro element is different from the substrate thermal expansivity, so silicon micro-resonance type accelerometer measuring accuracy temperature influence is remarkable.For the impact of compensation temperature on measurement result, common method is measure the environment temperature of silicon micro element and set up model of temperature compensation by outside temperature probe.Due to uncertainty and the heat conducting time delay that temperature field distributes, this compensation method poor effect and lag-effect is arranged.
Summary of the invention
Goal of the invention: in order to overcome the deficiencies in the prior art, the invention provides a kind of accelerometer self drive voltage signal of utilizing and silicon micro-resonance type accelerometer is carried out to the method for temperature compensation, by backoff algorithm, the accelerometer resonance frequency is exported and carried out accurate compensation in real time.
Technical scheme: for achieving the above object, the technical solution used in the present invention is:
A kind of silicon micro-resonance type accelerometer temperature compensation, comprise the steps:
(1) under without the acceleration signal input condition, in ℃ variation range of environment temperature-40~60, resonance frequency and driving DC voltage to silicon micro-resonance type accelerometer are measured, and obtain the temperature variant monotonic relationshi curve of resonance frequency and the temperature variant monotonic relationshi curve of driving DC voltage of resonance beam 1 and resonance beam 2; Described silicon micro-resonance type accelerometer has two resonance beam, is designated as respectively resonance beam 1 and resonance beam 2;
(2), under without the acceleration signal input condition, demarcate the monotone variation relation curve that resonance beam 1 maintains the constant driving DC voltage of resonance amplitude and its resonance frequency; Now the resonance frequency changing value of resonance beam 1 is the deviation frequency that temperature causes;
(3), under without the acceleration signal input condition, demarcate the monotone variation relation curve that resonance beam 2 maintains the constant driving DC voltage of resonance amplitude and its resonance frequency; Now the resonance frequency changing value of resonance beam 2 is the deviation frequency that temperature causes;
(4) use described silicon micro-resonance type accelerometer to carry out acceleration analysis, obtain the resonance frequency f of resonance beam 1
1resonance frequency f with resonance beam 2
2, and the driving DC voltage V of resonance beam 1 now
d1driving DC voltage V with resonance beam 2
d2;
(5) because the voltage signal antijamming capability is low, driving DC voltage is subject to noise, therefore to the driving DC voltage V of resonance beam 1 and resonance beam 2
d1and V
d2carry out filtering, the driving DC voltage after filtering noise is respectively
with
the monotone variation curve obtained according to step (3) obtains driving DC voltage
corresponding temperature drift frequency f
t1, the monotone variation curve obtained according to step (4) obtains driving DC voltage
corresponding temperature drift frequency f
t2;
(6) resonance frequency of resonance beam is the frequency f caused by acceleration signal
awith the frequency shift (FS) f caused by temperature
ttwo parts addition forms, that is:
f
1=f
a1+f
T1
f
2=f
a2+f
T2
Resonance beam 1 after the accounting temperature compensation and the difference on the frequency of resonance beam 2 are:
f
a1-f
a2=(f
1-f
T1)-(f
2-f
T2)=(f
1-f
2)-(f
T1-f
T2)
(7) calculate measured acceleration signal a
ccfor:
a
cc=(f
a1-f
a2)/S
F
S wherein
fconstant multiplier for accelerometer.
Described step (1) specifically comprises the steps:
(11), in ℃ variation range of environment temperature-40~60, demarcate s temperature spot;
(12) under without the acceleration signal input condition, test as follows: resonance frequency and the driving DC voltage of the resonance frequency of collection resonance beam 1 and driving DC voltage, collection resonance beam 2 on each temperature spot;
(13) experiment of repeated execution of steps (12), the experiment number of accumulative total execution step (12) is t time;
(14) resonance frequency under each temperature spot and driving DC voltage are made even and are:
Wherein, i=1,2 ..., s, j=1,2 ..., t; f
1i, jfor the resonance frequency that resonance beam 1 records during the j time repeated experiments on i temperature spot, f
2i, jfor the resonance frequency that resonance beam 2 records during the j time repeated experiments on i temperature spot, V
d1i, jfor the driving DC voltage that resonance beam 1 records during the j time repeated experiments on i temperature spot, V
d2i, jthe driving DC voltage recorded during the j time repeated experiments on i temperature spot for resonance beam 2;
(15), according to the corresponding relation of resonance frequency mean value, driving DC voltage mean value and temperature, obtain the temperature variant monotonic relationshi curve of resonance frequency and the temperature variant monotonic relationshi curve of driving DC voltage of resonance beam 1 and resonance beam 2.
Described step (2) specifically comprises the steps:
(21) to resonance beam 1, the average resonance frequencies under each temperature spot and average driving DC voltage data are used the cubic polynomial model of fit to carry out matching, obtain the monotone variation relation curve that resonance beam 1 maintains the constant driving DC voltage of resonance amplitude and its resonance frequency:
f
T1=a
0+a
1V
d1+a
2V
d1 2+a
3V
d1 3
(22) use the principle of least square, obtain the coefficient a of above formula
n, n=0,1,2,3.
Described step (3) specifically comprises the steps:
(31) to resonance beam 2, the average resonance frequencies under each temperature spot and average driving DC voltage data are used the cubic polynomial model of fit to carry out matching, obtain the monotone variation relation curve that resonance beam 2 maintains the constant driving DC voltage of resonance amplitude and its resonance frequency:
f
T2=b
0+b
1V
d2+b
2V
d2 2+b
3V
d2 3
(32) use the principle of least square, obtain the coefficient b of above formula
n, n=0,1,2,3.
The described measurement data V to driving DC voltage
dcarry out filtering to obtain
concrete grammar be:
At first, set up as drag:
Same driving DC voltage under same temperature spot is carried out to m actual value and measure, k=1,2 ..., m; V
d(k) be the driving DC voltage actual measured value measured for the k time,
for V
d(k) filtered value, ω (k) is the dynamic noise while measuring for the k time, υ (k) is the measurement noise of introducing in the k time measuring process, a, c is measuring system and the definite parameter of method of testing;
Secondly, by V
d(k) be expressed as V
d,k, will
be expressed as
variance yields according to following formula statistics dynamic noise ω (k) and measurement noise υ (k)
with
Then, use following recursion iterative, the measurement data of driving DC voltage carried out to filtering:
Wherein, b (k) is the time-variable filtering gain, and P (k) is equal square evaluated error.
Beneficial effect: silicon micro-resonance type accelerometer temperature compensation provided by the invention, overcome uncertainty and the hot conduction delay that in traditional direct temperature compensation method, temperature field distributes and brought the defect of relatively large deviation to compensation result, can realize real-time, high-precision temperature compensation; The temperature compensation cost of the inventive method is low, does not need additionally to increase sensor, only utilizes existing circuit devcie to realize.
The accompanying drawing explanation
Fig. 1 is structured flowchart of the present invention.
Embodiment
Below in conjunction with accompanying drawing, the present invention is further described.
A kind of silicon micro-resonance type accelerometer temperature compensation, comprise the steps:
(1) under without the acceleration signal input condition, in ℃ variation range of environment temperature-40~60, resonance frequency and driving DC voltage to silicon micro-resonance type accelerometer are measured, and obtain the temperature variant monotonic relationshi curve of resonance frequency and the temperature variant monotonic relationshi curve of driving DC voltage of resonance beam 1 and resonance beam 2; Described silicon micro-resonance type accelerometer has two resonance beam, is designated as respectively resonance beam 1 and resonance beam 2; Specifically comprise the steps:
(11), in ℃ variation range of environment temperature-40~60, demarcate s temperature spot; Such as, take 10 ℃ as temperature interval, p-40~60 ℃ of temperature ranges are divided, and obtain 11 temperature spots, i.e. s=11;
(12) under without the acceleration signal input condition, test as follows: resonance frequency and the driving DC voltage of the resonance frequency of collection resonance beam 1 and driving DC voltage, collection resonance beam 2 on each temperature spot; When gathering, can use temperature control device that the environment temperature of silicon micro-resonance type accelerometer is controlled on corresponding temperature spot;
(13) experiment of repeated execution of steps (12), the experiment number of accumulative total execution step (12) is t time;
(14) resonance frequency under each temperature spot and driving DC voltage are made even and are:
Wherein, i=1,2 ..., s, j=1,2 ..., t; f
1i, jfor the resonance frequency that resonance beam 1 records during the j time repeated experiments on i temperature spot, f
2i, jfor the resonance frequency that resonance beam 2 records during the j time repeated experiments on i temperature spot, V
d1i, jfor the driving DC voltage that resonance beam 1 records during the j time repeated experiments on i temperature spot, V
d2i, jthe driving DC voltage recorded during the j time repeated experiments on i temperature spot for resonance beam 2;
(15), according to the corresponding relation of resonance frequency mean value, driving DC voltage mean value and temperature, obtain the temperature variant monotonic relationshi curve of resonance frequency and the temperature variant monotonic relationshi curve of driving DC voltage of resonance beam 1 and resonance beam 2.
(2), under without the acceleration signal input condition, demarcate the monotone variation relation curve that resonance beam 1 maintains the constant driving DC voltage of resonance amplitude and its resonance frequency; Now the resonance frequency changing value of resonance beam 1 is the deviation frequency that temperature causes; Specifically comprise the steps:
(21) to resonance beam 1, the average resonance frequencies under each temperature spot and average driving DC voltage data are used the cubic polynomial model of fit to carry out matching, obtain the monotone variation relation curve that resonance beam 1 maintains the constant driving DC voltage of resonance amplitude and its resonance frequency:
f
T1=a
0+a
1V
d1+a
2V
d1 2+a
3V
d1 3
(22) use the principle of least square, obtain the coefficient a of above formula
n, n=0,1,2,3;
When inputting without acceleration, temperature is the reason that causes frequency shift, therefore be from the frequency of calculating of falling into a trap with above formula the deviation frequency that temperature causes.
(3), under without the acceleration signal input condition, demarcate the monotone variation relation curve that resonance beam 2 maintains the constant driving DC voltage of resonance amplitude and its resonance frequency; Now the resonance frequency changing value of resonance beam 2 is the deviation frequency that temperature causes; Specifically comprise the steps:
(31) to resonance beam 2, the average resonance frequencies under each temperature spot and average driving DC voltage data are used the cubic polynomial model of fit to carry out matching, obtain the monotone variation relation curve that resonance beam 2 maintains the constant driving DC voltage of resonance amplitude and its resonance frequency:
f
T2=b
0+b
1V
d2+b
2V
d2 2+b
3V
d2 3
(32) use the principle of least square, obtain the coefficient b of above formula
n, n=0,1,2,3;
When inputting without acceleration, temperature is the reason that causes frequency shift, therefore be from the frequency of calculating of falling into a trap with above formula the deviation frequency that temperature causes.
(4) use described silicon micro-resonance type accelerometer to carry out acceleration analysis, obtain the resonance frequency f of resonance beam 1
1resonance frequency f with resonance beam 2
2, and the driving DC voltage V of resonance beam 1 now
d1driving DC voltage V with resonance beam 2
d2.
(5) because the voltage signal antijamming capability is low, driving DC voltage is subject to noise, therefore to the driving DC voltage V of resonance beam 1 and resonance beam 2
d1and V
d2carry out filtering, the driving DC voltage after filtering noise is respectively
with
the monotone variation curve obtained according to step (3) obtains driving DC voltage
corresponding temperature drift frequency f
t1, the monotone variation curve obtained according to step (4) obtains driving DC voltage
corresponding temperature drift frequency f
t2.
(6) resonance frequency of resonance beam is the frequency f caused by acceleration signal
awith the frequency shift (FS) f caused by temperature
ttwo parts addition forms, that is:
f
1=f
a1+f
T1
f
2=f
a2+f
T2
Resonance beam 1 after the accounting temperature compensation and the difference on the frequency of resonance beam 2 are:
f
a1-f
a2=(f
1-f
T1)-(f
2-f
T2)=(f
1-f
2)-(f
T1-f
T2)。
(7) calculate measured acceleration signal a
ccfor:
a
cc=(f
a1-f
a2)/S
F
S wherein
fconstant multiplier for accelerometer.
Because the voltage signal antijamming capability is low, driving DC voltage is subject to noise, for fear of in frequency signal pointwise compensation process, by excessive voltage noise pull-in frequency measurement result, need to carry out filtering to the voltage signal collected in actual use procedure in step (4).This case is used following mode to carry out filtering, i.e. the described measurement data V to driving DC voltage
dcarry out filtering to obtain
concrete grammar be:
At first, set up as drag:
Same driving DC voltage under same temperature spot is carried out to m actual value and measure, k=1,2 ..., m; V
d(k) be the driving DC voltage actual measured value measured for the k time,
for V
d(k) filtered value, ω (k) is the dynamic noise while measuring for the k time, υ (k) is the measurement noise of introducing in the k time measuring process, a, c is measuring system and the definite parameter of method of testing;
Secondly, by V
d(k) be expressed as V
d,k, will
be expressed as
variance yields according to following formula statistics dynamic noise ω (k) and measurement noise υ (k)
with
Then, use following recursion iterative, the measurement data of driving DC voltage carried out to filtering:
Wherein, b (k) is the time-variable filtering gain, and P (k) is equal square evaluated error.
The above is only the preferred embodiment of the present invention; be noted that for those skilled in the art; under the premise without departing from the principles of the invention, can also make some improvements and modifications, these improvements and modifications also should be considered as protection scope of the present invention.
Claims (4)
1. a silicon micro-resonance type accelerometer temperature compensation, is characterized in that: comprise the steps:
(1) under without the acceleration signal input condition, in ℃ variation range of environment temperature-40~60, resonance frequency and driving DC voltage to silicon micro-resonance type accelerometer are measured, and obtain the temperature variant monotonic relationshi curve of resonance frequency and the temperature variant monotonic relationshi curve of driving DC voltage of resonance beam 1 and resonance beam 2; Described silicon micro-resonance type accelerometer has two resonance beam, is designated as respectively resonance beam 1 and resonance beam 2;
(2), under without the acceleration signal input condition, demarcate the monotone variation relation curve that resonance beam 1 maintains the constant driving DC voltage of resonance amplitude and its resonance frequency; Now the resonance frequency changing value of resonance beam 1 is the deviation frequency that temperature causes;
(3), under without the acceleration signal input condition, demarcate the monotone variation relation curve that resonance beam 2 maintains the constant driving DC voltage of resonance amplitude and its resonance frequency; Now the resonance frequency changing value of resonance beam 2 is the deviation frequency that temperature causes;
(4) use described silicon micro-resonance type accelerometer to carry out acceleration analysis, obtain the resonance frequency f of resonance beam 1
1resonance frequency f with resonance beam 2
2, and the driving DC voltage V of resonance beam 1 now
d1driving DC voltage V with resonance beam 2
d2;
(5) to the driving DC voltage V of resonance beam 1 and resonance beam 2
d1and V
d2carry out filtering, the driving DC voltage after filtering noise is respectively
with
the monotone variation curve obtained according to step (3) obtains driving DC voltage
corresponding temperature drift frequency f
t1, the monotone variation curve obtained according to step (4) obtains driving DC voltage
corresponding temperature drift frequency f
t2;
(6) resonance frequency of resonance beam is the frequency f caused by acceleration signal
awith the frequency shift (FS) f caused by temperature
ttwo parts addition forms, that is:
f
1=f
a1+f
T1
f
2=f
a2+f
T2
Resonance beam 1 after the accounting temperature compensation and the difference on the frequency of resonance beam 2 are:
f
a1-f
a2=(f
1-f
T1)-(f
2-f
T2)=(f
1-f
2)-(f
T1-f
T2)
(7) calculate measured acceleration signal a
ccfor:
a
cc=(f
a1-f
a2)/S
F
S wherein
fconstant multiplier for accelerometer.
2. silicon micro-resonance type accelerometer temperature compensation according to claim 1, it is characterized in that: described step (1) specifically comprises the steps:
(11), in ℃ variation range of environment temperature-40~60, demarcate s temperature spot;
(12) under without the acceleration signal input condition, test as follows: resonance frequency and the driving DC voltage of the resonance frequency of collection resonance beam 1 and driving DC voltage, collection resonance beam 2 on each temperature spot;
(13) experiment of repeated execution of steps (12), the experiment number of accumulative total execution step (12) is t time;
(14) resonance frequency under each temperature spot and driving DC voltage are made even and are:
Wherein, i=1,2 ..., s, j=1,2 ..., t; f
1i, jfor the resonance frequency that resonance beam 1 records during the j time repeated experiments on i temperature spot, f
2i, jfor the resonance frequency that resonance beam 2 records during the j time repeated experiments on i temperature spot, V
d1i, jfor the driving DC voltage that resonance beam 1 records during the j time repeated experiments on i temperature spot, V
d2i, jthe driving DC voltage recorded during the j time repeated experiments on i temperature spot for resonance beam 2;
(15), according to the corresponding relation of resonance frequency mean value, driving DC voltage mean value and temperature, obtain the temperature variant monotonic relationshi curve of resonance frequency and the temperature variant monotonic relationshi curve of driving DC voltage of resonance beam 1 and resonance beam 2.
3. silicon micro-resonance type accelerometer temperature compensation according to claim 2 is characterized in that:
Described step (2) specifically comprises the steps:
(21) to resonance beam 1, the average resonance frequencies under each temperature spot and average driving DC voltage data are used the cubic polynomial model of fit to carry out matching, obtain the monotone variation relation curve that resonance beam 1 maintains the constant driving DC voltage of resonance amplitude and its resonance frequency:
f
T1=a
0+a
1V
d1+a
2V
d1 2+a
3V
d1 3
(22) use the principle of least square, obtain the coefficient a of above formula
n, n=0,1,2,3;
Described step (3) specifically comprises the steps:
(31) to resonance beam 2, the average resonance frequencies under each temperature spot and average driving DC voltage data are used the cubic polynomial model of fit to carry out matching, obtain the monotone variation relation curve that resonance beam 2 maintains the constant driving DC voltage of resonance amplitude and its resonance frequency:
f
T2=b
0+b
1V
d2+b
2V
d2 2+b
3V
d2 3
(32) use the principle of least square, obtain the coefficient b of above formula
n, n=0,1,2,3.
4. silicon micro-resonance type accelerometer temperature compensation according to claim 3, is characterized in that: the described measurement data V to driving DC voltage
dcarry out filtering to obtain
concrete grammar be:
At first, set up as drag:
Same driving DC voltage under same temperature spot is carried out to m actual value and measure, k=1,2 ..., m; V
d(k) be the driving DC voltage actual measured value measured for the k time,
for V
d(k) filtered value, ω (k) is the dynamic noise while measuring for the k time, υ (k) is the measurement noise of introducing in the k time measuring process, a, c is measuring system and the definite parameter of method of testing;
Secondly, by V
d(k) be expressed as V
d,k, will
be expressed as
variance yields according to following formula statistics dynamic noise ω (k) and measurement noise υ (k)
with
Then, use following recursion iterative, the measurement data of driving DC voltage carried out to filtering:
Wherein, b (k) is the time-variable filtering gain, and P (k) is equal square evaluated error.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201310429703.1A CN103472259B (en) | 2013-09-18 | 2013-09-18 | Method for silicon micro-resonant type accelerometer temperature compensation |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201310429703.1A CN103472259B (en) | 2013-09-18 | 2013-09-18 | Method for silicon micro-resonant type accelerometer temperature compensation |
Publications (2)
Publication Number | Publication Date |
---|---|
CN103472259A true CN103472259A (en) | 2013-12-25 |
CN103472259B CN103472259B (en) | 2015-04-29 |
Family
ID=49797185
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201310429703.1A Active CN103472259B (en) | 2013-09-18 | 2013-09-18 | Method for silicon micro-resonant type accelerometer temperature compensation |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN103472259B (en) |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103869098A (en) * | 2014-04-16 | 2014-06-18 | 东南大学 | Silicon micro resonance type accelerometer circuit control system |
CN104535251A (en) * | 2015-01-12 | 2015-04-22 | 中国科学院电子学研究所 | Temperature self-compensating method and measuring mode for double-resonator pressure sensor |
CN107389979A (en) * | 2017-06-28 | 2017-11-24 | 东南大学 | The online temperature compensation of silicon micro-resonance type accelerometer based on resonant frequency |
CN108827346A (en) * | 2018-04-13 | 2018-11-16 | 南京理工大学 | Resonant transducer temperature-compensation method based on continuous ring-down |
CN108827804A (en) * | 2018-07-12 | 2018-11-16 | 浙江工业大学 | A kind of resonant mode fatigue tester dynamic load error online compensation method |
CN108931665A (en) * | 2018-05-21 | 2018-12-04 | 东南大学 | A kind of digital servo-control telemetry circuit for silicon micro-resonance type accelerometer |
CN109633205A (en) * | 2019-01-16 | 2019-04-16 | 南京理工大学 | A kind of quartz resonance accelerometer temperature compensation method |
CN110018330A (en) * | 2019-01-07 | 2019-07-16 | 东南大学 | Silicon micro-resonance type accelerometer temperature compensation algorithm based on adjustment structure compensation parameter |
CN111044758A (en) * | 2018-10-12 | 2020-04-21 | 苏州捷杰传感技术有限公司 | Acceleration sensor output value correction method and acceleration sensor |
CN111459211A (en) * | 2015-04-20 | 2020-07-28 | 深圳市大疆创新科技有限公司 | System and method for thermally regulating sensor operation |
CN114280328A (en) * | 2021-12-24 | 2022-04-05 | 西安交通大学 | MEMS resonant acceleration sensor based on symmetrical homomodal temperature compensation |
CN116147807A (en) * | 2023-04-24 | 2023-05-23 | 山东中科思尔科技有限公司 | Resonant pressure sensor modal compensation method, system, terminal and medium |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4155257A (en) * | 1977-05-23 | 1979-05-22 | The Singer Company | Temperature compensated vibrating beam accelerometer |
US5339698A (en) * | 1993-06-07 | 1994-08-23 | Alliedsignal Inc. | Vibrating beam force transducer with automatic adjustment of its electromagnetic drive |
CN102435774A (en) * | 2011-12-07 | 2012-05-02 | 浙江大学 | Temperature compensation system and method for capacitance type micro-mechanical accelerometer |
-
2013
- 2013-09-18 CN CN201310429703.1A patent/CN103472259B/en active Active
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4155257A (en) * | 1977-05-23 | 1979-05-22 | The Singer Company | Temperature compensated vibrating beam accelerometer |
US5339698A (en) * | 1993-06-07 | 1994-08-23 | Alliedsignal Inc. | Vibrating beam force transducer with automatic adjustment of its electromagnetic drive |
CN102435774A (en) * | 2011-12-07 | 2012-05-02 | 浙江大学 | Temperature compensation system and method for capacitance type micro-mechanical accelerometer |
Non-Patent Citations (3)
Title |
---|
GAVIN K. HO ET AL.: "TEMPERATURE COMPENSATED IBAR REFERENCE OSCILLATORS", 《MEMS 2006》, 31 January 2006 (2006-01-31), pages 910 - 913, XP010914394, DOI: 10.1109/MEMSYS.2006.1627948 * |
RALF ACHENBACH ET AL.: "A Digitally Temperature-Compensated Crystal Oscillator", 《IEEE JOURNAL OF SOLID-STATE CIRCUITS》, vol. 35, no. 10, 31 October 2000 (2000-10-31), pages 1502 - 1506, XP011061335 * |
顾广清等: "硅微陀螺仪数字化温度补偿系统的实现", 《舰船电子工程》, vol. 28, no. 12, 31 December 2008 (2008-12-31) * |
Cited By (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103869098B (en) * | 2014-04-16 | 2016-02-10 | 东南大学 | A kind of silicon micro-resonance type accelerometer circuit control system |
CN103869098A (en) * | 2014-04-16 | 2014-06-18 | 东南大学 | Silicon micro resonance type accelerometer circuit control system |
CN104535251A (en) * | 2015-01-12 | 2015-04-22 | 中国科学院电子学研究所 | Temperature self-compensating method and measuring mode for double-resonator pressure sensor |
CN104535251B (en) * | 2015-01-12 | 2017-02-22 | 中国科学院电子学研究所 | Temperature self-compensating method and measuring mode for double-resonator pressure sensor |
US11703522B2 (en) | 2015-04-20 | 2023-07-18 | SZ DJI Technology Co., Ltd. | Systems and methods for thermally regulating sensor operation |
CN111459211A (en) * | 2015-04-20 | 2020-07-28 | 深圳市大疆创新科技有限公司 | System and method for thermally regulating sensor operation |
CN111459211B (en) * | 2015-04-20 | 2022-07-15 | 深圳市大疆创新科技有限公司 | System and method for thermally regulating sensor operation |
CN107389979B (en) * | 2017-06-28 | 2019-07-12 | 东南大学 | The online temperature-compensation method of silicon micro-resonance type accelerometer based on resonance frequency |
CN107389979A (en) * | 2017-06-28 | 2017-11-24 | 东南大学 | The online temperature compensation of silicon micro-resonance type accelerometer based on resonant frequency |
CN108827346A (en) * | 2018-04-13 | 2018-11-16 | 南京理工大学 | Resonant transducer temperature-compensation method based on continuous ring-down |
CN108827346B (en) * | 2018-04-13 | 2020-10-20 | 南京理工大学 | Resonant sensor temperature compensation method based on continuous ring-down |
CN108931665A (en) * | 2018-05-21 | 2018-12-04 | 东南大学 | A kind of digital servo-control telemetry circuit for silicon micro-resonance type accelerometer |
CN108827804A (en) * | 2018-07-12 | 2018-11-16 | 浙江工业大学 | A kind of resonant mode fatigue tester dynamic load error online compensation method |
CN108827804B (en) * | 2018-07-12 | 2021-04-06 | 浙江工业大学 | Dynamic load error online compensation method for resonant fatigue testing machine |
CN111044758A (en) * | 2018-10-12 | 2020-04-21 | 苏州捷杰传感技术有限公司 | Acceleration sensor output value correction method and acceleration sensor |
CN110018330A (en) * | 2019-01-07 | 2019-07-16 | 东南大学 | Silicon micro-resonance type accelerometer temperature compensation algorithm based on adjustment structure compensation parameter |
CN109633205A (en) * | 2019-01-16 | 2019-04-16 | 南京理工大学 | A kind of quartz resonance accelerometer temperature compensation method |
CN114280328A (en) * | 2021-12-24 | 2022-04-05 | 西安交通大学 | MEMS resonant acceleration sensor based on symmetrical homomodal temperature compensation |
CN114280328B (en) * | 2021-12-24 | 2022-09-13 | 西安交通大学 | MEMS resonant acceleration sensor based on symmetrical homomodal temperature compensation |
CN116147807A (en) * | 2023-04-24 | 2023-05-23 | 山东中科思尔科技有限公司 | Resonant pressure sensor modal compensation method, system, terminal and medium |
Also Published As
Publication number | Publication date |
---|---|
CN103472259B (en) | 2015-04-29 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN103472259B (en) | Method for silicon micro-resonant type accelerometer temperature compensation | |
CN104406846B (en) | Measurement system and measurement method for stress waves of Hopkinson bars by using flexoelectric effect | |
CN102621225B (en) | Method for testing damping characteristic parameter of road surface and bridge deck pavement material | |
CN108535511B (en) | FM accelerometer force balance detection method based on static negative stiffness frequency calculation | |
CN105424160A (en) | Method for realizing blade synchronous vibration parameter identification | |
CN104573248A (en) | EMD based fiber-optic gyroscope temperature drift multi-scale extreme learning machine training method | |
CN107389979B (en) | The online temperature-compensation method of silicon micro-resonance type accelerometer based on resonance frequency | |
CN105043348A (en) | Accelerometer gyroscope horizontal angle measurement method based on Kalman filtering | |
CN104819710B (en) | A kind of resonant micromechanical silicon gyro with temperature compensation structure | |
CN105571612A (en) | Automatic testing method for key parameters of MEMS gyroscope structure | |
CN106932125B (en) | Compensation method of silicon resonance pressure sensor | |
CN107300433A (en) | A kind of method that utilization piezoelectric force transducer measures static force | |
CN105758421A (en) | Fiber-optic gyroscope eigenfrequency measuring equipment and application thereof | |
CN204255494U (en) | Bridge vibration monitoring device | |
CN115435768A (en) | Hemispherical resonant gyroscope temperature modeling compensation method based on real-time sliding window | |
CN104820757A (en) | Temperature drift property neural network modeling method of MEMS (Micro Electro Mechanical Systems) top on the basis of physical model | |
CN104020259A (en) | Testing device and testing method for coupling relationship between loss factors of damping material and energy as well as temperature | |
CN103245846B (en) | Dynamic zero drift filtering algorithm for relay protection | |
CN104678126A (en) | Phase-shift temperature compensation method based on parasitic resistance for micro-mechanical capacitive accelerometer | |
CN103532530A (en) | Pulse peak detection device | |
CN103699010B (en) | A kind of servo system identification method based on relay position feedback temporal signatures | |
CN101793569A (en) | Method for measuring temperature of sensitive devices of quartz micro-machined gyroscopes and temperature compensation circuit | |
CN104765075A (en) | Dual-optical-path testing device for light speed limited effect in absolute gravimeter | |
CN104713573A (en) | Method for measuring diffraction loss of laser gyro | |
CN201306979Y (en) | Device for improving strapdown inertial temperature error compensation precision |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C14 | Grant of patent or utility model | ||
GR01 | Patent grant |