CN101881784B - Position and speed measuring device based on inductosyn or rotary transformer - Google Patents

Position and speed measuring device based on inductosyn or rotary transformer Download PDF

Info

Publication number
CN101881784B
CN101881784B CN2010101988710A CN201010198871A CN101881784B CN 101881784 B CN101881784 B CN 101881784B CN 2010101988710 A CN2010101988710 A CN 2010101988710A CN 201010198871 A CN201010198871 A CN 201010198871A CN 101881784 B CN101881784 B CN 101881784B
Authority
CN
China
Prior art keywords
omega
information
speed
theta
phase
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.)
Expired - Fee Related
Application number
CN2010101988710A
Other languages
Chinese (zh)
Other versions
CN101881784A (en
Inventor
张�育
王跃明
刘银年
王建宇
王晟伟
庄晓琼
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shanghai Institute of Technical Physics of CAS
Original Assignee
Shanghai Institute of Technical Physics of CAS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Shanghai Institute of Technical Physics of CAS filed Critical Shanghai Institute of Technical Physics of CAS
Priority to CN2010101988710A priority Critical patent/CN101881784B/en
Publication of CN101881784A publication Critical patent/CN101881784A/en
Application granted granted Critical
Publication of CN101881784B publication Critical patent/CN101881784B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Transmission And Conversion Of Sensor Element Output (AREA)

Abstract

The invention discloses a position and speed measuring device based on an inductosyn or a rotary transformer. The device adopts a phase discrimination type processing method and comprises an exciting circuit, an inductosyn or a rotary transformer, a signal processing circuit and a central processing unit. An exciting signal is generated by the exciting circuit and subject to power amplification, a power signal passes through the inductosyn or the rotary transformer, the signal processing circuit carries out filtering, amplification, phase shift and reshaping on the power signal, and then the processed signal is sent to the central processing unit. The central processing unit obtains position information through the phase information of a signal, obtains speed information through a position information difference, obtains acceleration information through a speed information difference, and carries out dynamic error correction on phase or speed according to speed and acceleration information. The invention is simple to realize, has low cost and high accuracy, is suitable for both a high-speed operation condition and a low-speed operation condition, and can be applied to the fields of aerospace, military, industry and the like to realize dynamic position and speed measurement.

Description

A kind of position and velocity measuring device based on inductosyn or rotary transformer
Technical field
The present invention relates to the measuring technique of speed, position, more particularly, the present invention relates to a kind of position and velocity measuring device based on inductosyn or rotary transformer.
Background technology
Inductosyn and rotary transformer all are to utilize electromagnetic principle to convert displacement of the lines or angular displacement the sensor of electric signal to, and the collocation driving circuit can go out positional information by the amplitude or the phase extraction of electric signal, and two kinds of sensors have identical principle of work.Because the principle of work of inductosyn and rotary transformer is based under the static situation designed, therefore no matter be according to the amplitude discrimination type or the measurement mechanism of phase demodulating type method manufacturing, in mobile or rotation process, all dynamic error can be occurred, even miscount can be caused.
Wherein the phase demodulating type method is as " Harbin University of Science and Technology's journal " method that February in 2003, the 8th volume the 1st phase 12-14 page or leaf " systematic study of a phase demodulating type inductosyn dynamic measuring angle " literary composition was discussed, according to the measurement mechanism of its principle manufacturing as shown in Figure 1, comprise exciting circuit, inductosyn or rotary transformer, signal processing circuit, CPU (central processing unit), excited signal is by the exciting circuit generation and carry out power amplification, after power signal passes through inductosyn or rotary transformer, carry out filtering by signal processing circuit, amplify, phase shift, the signal that obtains is shown in (1) formula:
e = k ( 1 - ω t ω 0 ) sin ( ω 0 t - θ t ) - - - ( 1 )
Wherein k is a constant, θ tBe signal phase, represented the mechanical angle that turns in segmentation cycle, ω tBe the speed of inductosyn or rotary transformer motion, ω 0Be the excited signal angular frequency.(1) signal e is identified its phase information and is obtained positional information by CPU (central processing unit) through after the shaping in the formula, and obtains velocity information by the positional information difference, and the process flow diagram of CPU (central processing unit) internal program computing as shown in Figure 2.According to the measurement mechanism of this method manufacturing, its advantage is: need not produce tracking signal or carry out multiplying, therefore than amplitude discrimination type method realize convenient, cost is low.Weak point is: because the mechanical angle of motion itself also is a variations per hour, when rotating, can cause the variation of signal frequency, and shown in (2) formula,
e = k ( 1 - ω t ω 0 ) sin [ ω 0 t - ω t t - θ t ′ ]
= k ( 1 - ω t ω 0 ) sin [ ( 1 - ω t ω 0 ) ω 0 t - θ t ′ ] - - - ( 2 )
The phase information θ that identifies by (2) formula t' and the mechanical angle of actual process is also unequal, brings dynamic error, can make that simultaneously saltus step appears in measurement result when inductosyn turns over zero point in segmentation cycle, as shown in Figure 3, and makes speed calculation mistake occur in this sampling period, as shown in Figure 4.
Summary of the invention
Based on the problems referred to above, the objective of the invention is to design a kind of simple in structure, with low cost, position and velocity measuring device that accuracy is high based on inductosyn or rotary transformer.
The present invention is the improvement of phase demodulating type measurement mechanism, comprise exciting circuit, inductosyn or rotary transformer, signal processing circuit, CPU (central processing unit), excited signal is by the exciting circuit generation and carry out power amplification, after power signal passes through inductosyn or rotary transformer, undertaken sending into CPU (central processing unit) after filtering, amplification, phase shift, the shaping by signal processing circuit, the treatment step of CPU (central processing unit) internal program is:
1) phase information of identification signal;
2) judge whether to carry out the phase place correction, revise, then revise with following formula as needs:
θ t ′ = θ t ( 1 + ω t ω 0 )
Or
θ t ′ = θ t ( 1 + ω t ω 0 - ω t )
Or
θ t ′ = θ t [ 1 + ω t ω 0 - ω t + θ t a ω t ( ω 0 - ω t ) 3 ]
θ wherein t' be revised phase information, θ tBe the phase information before revising, ω 0Be excited signal angular frequency, ω tBe present speed, a is a current acceleration;
3) obtain positional information by phase information, and set up storehouse, the degree of depth of storehouse is more than 2 or 2;
4) judge whether to carry out position correction, as need not to revise, current location information is pushed on, revise, then revise according to the following steps as needs, its process flow diagram as shown in Figure 5:
A) judge the direction that moves or rotate, identical with the phase place growing direction as direction of motion then is forward, otherwise then is reverse;
B) when counter motion, judge that whether this sampling period is through zero crossing, as without zero point, then the positional information that this sampling period is extracted pushes on, as through zero crossing, then two positional informations are pushed on successively, first is a pairing positional value at this zero point, and second is the positional value that extracts in the current sampling period;
C) when positive movement, judge whether this sampling period extract phase information, if can extract, then the positional information that this sampling period is extracted pushes on, as can not extract phase information, and this sampling period is not done any operation;
5) obtain velocity information by the positional information difference in the storehouse;
6) judge whether to carry out the speed correction, revise, then revise with following formula as needs:
ω t ′ = ω t ( 1 + ω t ω 0 )
Or
ω t ′ = ω t ( 1 + ω t ω 0 - ω t )
Or
ω t ′ = ω t ( 1 + ω t ω 0 - ω t ) + a θ t ω 0 ( ω 0 - ω t ) 2
Or
ω t ′ = ω t ( 1 + ω t ω 0 - ω t ) + a θ t ω 0 2 - ω 0 ω t + 2 ω t 2 ( ω 0 - ω t ) 3
ω wherein t' be revised speed, ω tBe the speed before revising;
7) the velocity information difference that was obtained by a present speed information and a last sampling period obtains acceleration information, and degree of will speed up information is used for the correction to phase place and speed.
CPU (central processing unit) to the Signal Processing flow process as shown in Figure 6.
The present invention has inherited existing phase demodulating type apparatus structure advantage simple, with low cost, also has higher dynamic accuracy simultaneously, and the speed calculation mistake can not occur through zero point in segmentation cycle the time.
It below is the proof of correction algorithm.For better understanding the principle of correction algorithm, as shown in Figure 7 with the signal waveform modeling that observed on the oscillograph.It is ω with speed that the inductosyn output signal is regarded as one tThe motion object, and sampling thief initially return in each cycle once sampled result and with ω 0Speed begin to catch up with it, when the two meets, with the position of meeting as sampled result, the quantification progression D=f of sampled result c/ f 0, promptly each DN value is represented the electric segmentation angle of 2 π/D, wherein ω tBe inductosyn speed, ω 0Be excited signal angular frequency, f cBe sample frequency, f 0Be the excited signal frequency.Like this, system just has been transformed into the problem of meeting of two objects to signals sampling, and sample frequency then just causes quantization error to the differentiation of Encounter Time, and we claim this model to be the model that meets.Be without loss of generality, the acceleration of supposing inductosyn is α, and the even rotation of quickening is done by system in the same sampling period.In addition, owing to quantize, the full scale sampling has only (D-1)/D cycle, thus system forward and reverse pass through inductosyn during zero point situation slightly different.
When antiport, suppose T 0In time, is engraved in the initial position in certain sampling period and samples first rising edge, owing to should just just begin in the sampling period this moment, and system will just can return sampled result after the sampling period finishes, therefore behind one-period nearly promptly at T 0+ Δ T returns the result 0 of this time sampling constantly and begins new round sampling.This moment, inductosyn passed through-ω tΔ T-α Δ T 2/ 2 displacement, wherein Δ T=2 π/ω 0Be the sampling period.So, according to the model that meets, the time that rising edge experienced that next time samples signal satisfies:
2 π - ω t ΔT - 1 2 αΔ T 2 = ( ω 0 + ω t + αΔT ) t + 1 2 α t 2
Separate this equation and omit high-order term and get:
t 1 = ω 0 - ω t ω 0 + ω t ΔT - 16 α π 2 ( ω 0 + ω t ) 3
≈ ΔT - - - ( 3 )
From (3) formula as can be seen, acceleration alpha only has influence on the cubic term of result of calculation, therefore can temporarily ignore situation about only considering at the uniform velocity.In this time, the current sampling period finishes soon, and system will return when time sampled result at once.That is to say, at T 0+ 2 Δ T constantly, when system returned for the second time sampled result, inductosyn reality had turned over-2 ω approximately tThe angle of Δ T, and system can only judge by accident-ω tThe angle of Δ T, error-ω tΔ T.The model of system is shown in Fig. 7 (a).
When forward turns round, suppose at T 0Constantly, sample the rising edge of signal in the last moment of certain one-period, and at T 0+ Δ t returns the D-1 as a result of this time sampling constantly, begins new round sampling simultaneously.This moment, inductosyn passed through ω tΔ t+ α Δ t 2/ 2 displacement, wherein Δ t=Δ T/D is a sampling interval.So, according to the model that meets, sample the needed time of system's rising edge satisfies next time:
2 π D - 1 D + ω t Δt + 1 2 α Δt 2 = ( ω 0 - ω t - αΔt ) t - 1 2 α t 2
Separate this equation and omit high-order term and get:
t 2 = ω 0 ω 0 - ω t ΔT + Δt + 4 α π 2 ( ω 0 - ω t ) 3
> ΔT - - - ( 4 )
From (4) formula as can be seen, angular acceleration still in the cubic term of result of calculation, can temporarily be ignored, and only considers situation at the uniform velocity.This moment, the inductosyn signal entered next cycle, can not meet with sampled signal in this cycle.Changing a kind of saying is exactly that the inductosyn output signal frequency is greater than f 0, and the zero clearing again of this hour counter.Sampling thief may return last sampled result D-1 like this, also may return a result 0, and this depends on the setting of system itself.Supposing the system is to return last sampled result, and will judge inductosyn so by accident is static at this moment, and in fact inductosyn has turned over about ω tThe angle of Δ T, error ω tΔ T.At this moment system model is shown in Fig. 7 (b).
According to the analysis of front, for the system of uniform rotation, dynamic error can be accumulated to maximal value and reach (p/360) (ω when being about to by zero point t/ ω 0), wherein p is the inductosyn number of pole-pairs.In all the other angles, error should have following form so:
Δ θ t 1 ′ = - θ t ω t ω 0 - - - ( 5 )
(5) formula is a modifying factor of dynamic error, and (2) formula then becomes like this:
e = k sin [ ( 1 - ω t ω 0 ) ω 0 t - θ t ( t ) + ∫ 0 t θ t ( t ) ω t ( t ) ω 0 dt ] - - - ( 6 )
Can release the error of correction algorithm by (3), (4) and (5) formula, at first consider the situation of uniform rotation:
| Δ θ t ′ ′ | ≤ | ΔT - ω 0 - ω t ω 0 + ω t ΔT | · 2 π ω t ω 0 / 2 ΔT
= 2 π ω t 2 ( ω 0 + ω t ) ω 0 - - - ( 7 )
(7) formula is to be obtained by (3) formula and (5) formula, because actually when inductosyn is discussed oppositely by zero point considered two sampling periods, and therefore will be divided by 2 Δ T.Simultaneously, can obtain by (4) formula and (5) formula
| Δ θ t ′ ′ | ≤ | ΔT - ω 0 ω 0 - ω t ΔT - Δt | · 2 π ω t ω 0 / ΔT
= | 2 π ω t 2 ( ω 0 - ω t ) ω 0 + 2 π ω t D ω 0 | - - - ( 8 )
If sample frequency is enough high, can regard D → ∞ as, (8) formula then becomes so
| Δ θ t ′ ′ | ≤ 2 π ω t 2 ( ω 0 - ω t ) ω 0 - - - ( 9 )
After considering direction, (7) formula has identical form with (9) formula.The error that adds this two formula, (5) formula should be modified to:
Δ θ t 2 ′ = - θ t ω t ω 0 - θ t ω t 2 ( ω 0 - ω t ) ω 0
= - θ t ω t ω 0 - ω t - - - ( 10 )
Under the situation of variable motion, need to add the cubic term in (3) formula and (4) formula.Because (3) formula has been analyzed the situation in two sampling periods, square after and the cubic term of (4) formula 4 times relation is arranged.Therefore, in conjunction with the form of (7), (9) and (10) formula, the modifying factor in the time of can releasing variable motion is:
Δ θ t 3 ′ = - θ t ω t ω 0 - ω t - θ t 2 a ω t ( ω 0 - ω t ) 3 - - - ( 11 )
(5) formula, (10) formula and (11) formula be respectively the phase place dynamic error once, secondary and three modifying factors.Respectively to (5) formula, (10) formula and (11) formula differentiate can obtain the speed dynamic error once, secondary and three modifying factors are:
Δ ω t 1 = - ω t ω t ω 0 - θ t a ω 0
≈ - ω t ω t ω 0 - - - ( 12 )
Δ ω t 2 = - ω t ω t ω 0 - ω t - θ t a ω 0 ( ω 0 - ω t ) 2
≈ - ω t ω t ω 0 - ω t - - - ( 13 )
Δ ω t 3 = - ω t ω t ω 0 - ω t - θ t a ω 0 ( ω 0 - ω t ) 2 - 2 ω t θ t a ω t ( ω 0 - ω t ) 3 - θ t 2 a 2 ( ω 0 + 2 ω t ) ( ω 0 - ω t ) 4
≈ - ω t ω t ω 0 - ω t - a θ t ω 0 2 - ω 0 ω t + 2 ω t 2 ( ω 0 - ω t ) 3
≈ - ω t ω t ω 0 - ω t - a θ t ω 0 ( ω 0 - ω t ) 2
(14)
For position and velocity accuracy the system of requirement is arranged all, only need that phase place is carried out the dynamic error correction and get final product, with position and speed that revised phasometer is calculated, its dynamic error is corrected.And not high but to position accuracy demand to the demanding system of velocity accuracy, can only carry out the dynamic error correction and do not need the position is revised speed.Traditional rate algorithm only writes down a positional information that extracts in the past, and obtains speed with the current positional information difference that extracts, and this method does not have immunity to position sudden change shown in Figure 2, causes the speed calculation mistake.For obtaining continuous position information, need carry out interpolation processing, also need to write down at least simultaneously the positional information that two or more extract in the past.Interpolation processing is equivalent to the zero degree correction to speed, is particularly useful for this system that is bad at the chip of floating-point operation as central processing element with FPGA, and angle information reduces greatly through its dynamic error of velocity information that calculates after the interpolation processing.The present invention uses the method recording angular information of storehouse, so the degree of depth of storehouse is more than 2 or 2, and the used positional information of computing velocity is extracted in storehouse, the processing that once pushes on of cycle of promptly extracting phase place or position in each sampling period.The step of interpolation algorithm and being contemplated that:
A) judge the direction that moves or rotate, identical with the phase place growing direction as direction of motion then is forward, otherwise then is reverse.
B) when counter motion, because of signal frequency becomes greatly, the cycle shortens, and need insert a positional information in a segmentation cycle, this positional information is pairing position at this segmentation zero point in cycle.Therefore need whether judge this sampling period that as without zero point, then the positional information with the extraction of this sampling period pushes on through zero crossing; As through zero crossing, then two positional informations are pushed on successively, first is a pairing positional value at this zero point, second is the positional value that extracts in the current sampling period.
C) when positive movement, because of signal frequency diminishes, the cycle is elongated, last interior sampling period of segmentation cycle can not extracted phase information, and the positional information of register memory storage is the positional information of extracting in a last sampling period, need throw away this wrong positional information.Therefore need judge whether this sampling period extract phase information, if can extract that then the positional information with the extraction of this sampling period pushes on; As can not extract phase information, and expression is about to through zero crossing, and this sampling period is not done any operation, promptly is equivalent to throw away the positional information of a mistake.
The process flow diagram of the interpolation and the algorithm that pushes on as shown in Figure 4.
Description of drawings
Fig. 1 is based on the measurement mechanism basic structure block diagram of inductosyn or rotary transformer.
Fig. 2 tradition phase demodulating type measurement mechanism CPU (central processing unit) program flow diagram.
Positional information saltus step synoptic diagram during Fig. 3 tradition phase demodulating type measurement mechanism zero crossing.
Speed miscount synoptic diagram during Fig. 4 tradition phase demodulating type measurement mechanism zero crossing.
Fig. 5 interpolation stack algorithm of the present invention process flow diagram.
Fig. 6 CPU (central processing unit) program flow diagram of the present invention.
Fig. 7 dynamic error correction algorithm of the present invention model.
Embodiment
The present invention includes exciting circuit, inductosyn or rotary transformer, signal processing circuit, CPU (central processing unit), excited signal is by the exciting circuit generation and carry out power amplification, after power signal passes through inductosyn or rotary transformer, undertaken sending into CPU (central processing unit) after filtering, amplification, phase shift, the shaping by signal processing circuit, the treatment step of CPU (central processing unit) internal program is:
1) phase information of identification signal;
2) judge whether to carry out the phase place correction, also there is requirement the position as system when the kinetic measurement, then need earlier phase place to be revised, correction formula is derived by (5), (10), (11) formula:
θ t ′ = θ t ( 1 + ω t ω 0 ) - - - ( 15 )
Or
θ t ′ = θ t ( 1 + ω t ω 0 - ω t ) - - - ( 16 )
Or
θ t ′ = θ t [ 1 + ω t ω 0 - ω t + θ t a ω t ( ω 0 - ω t ) 3 ] - - - ( 17 )
θ wherein t' be revised phase information, θ tBe the phase information before revising, ω 0Be excited signal angular frequency, ω tBe present speed, a is a current acceleration, and above formula is selected one according to the system design index, the error maximum of (15) formula, the error minimum of (17) formula;
3) obtain positional information by phase information, and set up storehouse, the degree of depth of storehouse is more than 2 or 2;
4) judge whether to carry out position correction,, then need not to carry out again position correction as phase place being revised before; As need not to revise, current location information is pushed on, revise as needs, then revise according to the following steps, its process flow diagram as shown in Figure 4:
A) judge the direction that moves or rotate, identical with the phase place growing direction as direction of motion then is forward, otherwise then is reverse;
B) when counter motion, judge that whether this sampling period is through zero crossing, as without zero point, then the positional information that this sampling period is extracted pushes on, as through zero crossing, then two positional informations are pushed on successively, first is a pairing positional value at this zero point, second is the positional value that extracts in the current sampling period
C) when positive movement, judge whether this sampling period extract phase information, if can extract, then the positional information that this sampling period is extracted pushes on, as can not extract phase information, and this sampling period is not done any operation;
5) obtain velocity information by the positional information difference in the storehouse;
6) judge whether to carry out the speed correction,, then need not speed is revised as phase place being revised before; As correction being carried out in the position before, then can revise speed, can not revise yet, depend on the system design index, high as the speed dynamic accuracy is required, then need to carry out the speed correction; Revise as needs, then revise with following formula:
ω t ′ = ω t ( 1 + ω t ω 0 ) - - - ( 18 )
Or
ω t ′ = ω t ( 1 + ω t ω 0 - ω t ) - - - ( 19 )
Or
ω t ′ = ω t ( 1 + ω t ω 0 - ω t ) + a θ t ω 0 ( ω 0 - ω t ) 2 - - - ( 20 )
Or
ω t ′ = ω t ( 1 + ω t ω 0 - ω t ) + a θ t ω 0 2 - ω 0 ω t + 2 ω t 2 ( ω 0 - ω t ) 3 - - - ( 21 )
ω wherein t' be revised speed, ω tBe the speed before revising, above formula is selected one according to the system design index, the error maximum of (18) formula, the error minimum of (21) formula;
7) the velocity information difference that was obtained by a present speed information and a last sampling period obtains acceleration information, and degree of will speed up information is used for the correction to phase place and speed.
CPU (central processing unit) to the Signal Processing flow process as shown in Figure 5.

Claims (1)

1. position and speed measurement method based on an inductosyn or a rotary transformer, adopt the phase demodulating type disposal route, comprise exciting circuit, inductosyn or rotary transformer, signal processing circuit, CPU (central processing unit), excited signal is by the exciting circuit generation and carry out power amplification, after power signal passes through inductosyn or rotary transformer, undertaken sending into CPU (central processing unit) after filtering, amplification, phase shift and the shaping by signal processing circuit, it is characterized in that: the step of described CPU (central processing unit) internal program operation is:
1) phase information of identification signal;
2) judge whether to carry out the phase place correction, revise, then revise with following formula as needs:
θ t ′ = θ t ( 1 + ω t ω 0 )
Or
θ t ′ = θ t ( 1 + ω t ω 0 - ω t )
Or
θ t ′ = θ t [ 1 + ω t ω 0 - ω t + θ t a ω t ( ω 0 - ω t ) 3 ]
θ wherein t' be revised phase information, θ tBe the phase information before revising, ω 0Be excited signal angular frequency, ω tBe present speed, a is a current acceleration;
3) obtain positional information by phase information, and set up storehouse, the degree of depth of storehouse is more than 2;
4) judge whether to carry out position correction, as need not to revise, current location information is pushed on, revise, then revise according to the following steps as needs:
A) judge the direction that moves or rotate, identical with the phase place growing direction as direction of motion then is forward, otherwise then is reverse;
B) when counter motion, judge that whether this sampling period is through zero crossing, as without zero point, then the positional information that this sampling period is extracted pushes on, as through zero crossing, then two positional informations are pushed on successively, first is a pairing positional value at this zero point, and second is the positional value that extracts in the current sampling period;
C) when positive movement, judge whether this sampling period extract phase information, if can extract, then the positional information that this sampling period is extracted pushes on, as can not extract phase information, and this sampling period is not done any operation;
5) obtain velocity information by the positional information difference in the storehouse;
6) judge whether to carry out the speed correction, revise, then revise with following formula as needs:
ω t ′ = ω t ( 1 + ω t ω 0 )
Or
ω t ′ = ω t ( 1 + ω t ω 0 - ω t )
Or
ω t ′ = ω t ( 1 + ω t ω 0 - ω t ) + a θ t ω 0 ( ω 0 - ω t ) 2
Or
ω t ′ = ω t ( 1 + ω t ω 0 - ω t ) + a θ t ω 0 2 - ω 0 ω t + 2 ω t 2 ( ω 0 - ω t ) 3
ω wherein t' be revised speed, ω tBe the speed before revising;
7) the velocity information difference that was obtained by a present speed information and a last sampling period obtains acceleration information, and degree of will speed up information is used for the correction to phase place and speed.
CN2010101988710A 2010-06-11 2010-06-11 Position and speed measuring device based on inductosyn or rotary transformer Expired - Fee Related CN101881784B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2010101988710A CN101881784B (en) 2010-06-11 2010-06-11 Position and speed measuring device based on inductosyn or rotary transformer

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2010101988710A CN101881784B (en) 2010-06-11 2010-06-11 Position and speed measuring device based on inductosyn or rotary transformer

Publications (2)

Publication Number Publication Date
CN101881784A CN101881784A (en) 2010-11-10
CN101881784B true CN101881784B (en) 2011-09-14

Family

ID=43053845

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2010101988710A Expired - Fee Related CN101881784B (en) 2010-06-11 2010-06-11 Position and speed measuring device based on inductosyn or rotary transformer

Country Status (1)

Country Link
CN (1) CN101881784B (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10274988B2 (en) * 2014-11-19 2019-04-30 Panasonic Intellectual Property Management Co., Ltd. Input/output operation device
CN105628050A (en) * 2016-03-29 2016-06-01 安徽中电兴发与鑫龙科技股份有限公司 Circuit structure of speed odometer
CN108731703B (en) * 2018-06-05 2020-11-06 上海麦歌恩微电子股份有限公司 Angle sensor and rotation direction inversion delaying method of rotary encoder

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2141235A (en) * 1983-06-09 1984-12-12 Evershed Power Optics Position measurement
CN1083585A (en) * 1992-09-02 1994-03-09 陆启湘 A kind of induction synchronizer digital display displacement measuring method
CN101545915A (en) * 2009-04-30 2009-09-30 中国科学院上海技术物理研究所 Motor speed measuring method based on Doppler effect of inductosyn

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2141235A (en) * 1983-06-09 1984-12-12 Evershed Power Optics Position measurement
CN1083585A (en) * 1992-09-02 1994-03-09 陆启湘 A kind of induction synchronizer digital display displacement measuring method
CN101545915A (en) * 2009-04-30 2009-09-30 中国科学院上海技术物理研究所 Motor speed measuring method based on Doppler effect of inductosyn

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
徐凤霞等.鉴相型感应同步器动态测角***研究.《哈尔滨理工大学学报》.2003,第8卷(第1期),12-14. *
谢仁飚等.方波激磁的感应同步器驱动及信号处理技术.《中国惯性技术学报》.2008,第16卷(第3期),368-370,374. *

Also Published As

Publication number Publication date
CN101881784A (en) 2010-11-10

Similar Documents

Publication Publication Date Title
CN107391818B (en) A kind of Vibrating modal parameters recognition methods based on state observer
CN201594092U (en) Novel vehicular speed and range measuring equipment with multiple sensors
CN106499957B (en) A kind of pressure wave signal generator and in-pipeline detector real-time tracking localization method
CN103616710A (en) Multi-sensor combined navigation time synchronizing system based on field programmable gate array (FPGA)
CN103177584B (en) Vehicle speed detection method based on enumeration probe
EP1498698A3 (en) Compensation method of resolver detected position
CN101881784B (en) Position and speed measuring device based on inductosyn or rotary transformer
CN103714045A (en) Information fusion estimation method for asynchronous multi-rate non-uniform sampled observation data
CN110806193A (en) Subway tunnel deformation detection system
CN102818556A (en) Vehicle road gradient detection method and device thereof
CN101545915B (en) Motor speed measuring method based on Doppler effect of inductosyn
CN104197958A (en) Speedometer calibration method based on laser velocimeter dead reckoning system
CN110501516A (en) Combination velocity-measuring system and method for ultrahigh speed linear motor
CN100514068C (en) Method for measuring rotating speed of rotating shaft by sliding time window method
CN104142624B (en) Time synchronization method and system based on waveform matching
CN101782964B (en) Weight loss feather extraction method based on acceleration transducer
CN114444284A (en) Method and system for generating road base map of real-time simulation scene at vehicle end
CN102706365A (en) Calibration method for three-beam laser velocimeter on basis of navigation system
CN104361650A (en) Method for automatically calibrating pulse factor of vehicle traveling data recorder
CN103364842A (en) Error separation method of strapdown airborne gravitometer
CN109204321A (en) Signal processing method, sliding detection method, the control method of vehicle and device
CN101976300B (en) Variable weight fusion method for altitude channel identification data of unmanned helicopter
CN103605128B (en) A kind of speed-measuring method and device
CN106052744B (en) Pipeline airvey system minimum pressure drop speed determination method based on electrostatic transducer
CN104217001B (en) A kind of adaptive wheel speed calculation method of vehicle based on XML tree

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
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20110914

Termination date: 20140611

EXPY Termination of patent right or utility model