CN102519449B - Fiber optic gyro (FOG) signal denoising method based on overlap M-band discrete wavelet transform (OMDWT) - Google Patents

Fiber optic gyro (FOG) signal denoising method based on overlap M-band discrete wavelet transform (OMDWT) Download PDF

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CN102519449B
CN102519449B CN201110425096.2A CN201110425096A CN102519449B CN 102519449 B CN102519449 B CN 102519449B CN 201110425096 A CN201110425096 A CN 201110425096A CN 102519449 B CN102519449 B CN 102519449B
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崔培玲
张会娟
全伟
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Beihang University
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Abstract

The invention relates to a fiber optic gyro (FOG) signal denoising method based on overlap M-band discrete wavelet transform (OMDWT). The FOG signal denoising method comprises the following steps of: establishing an FOG output signal model at first; carrying out OMDWT wavelet decomposition on an FOG output signal; then carrying out threshold processing on an OMDWT wavelet coefficient; and finally carrying out OMDWT wavelet reconstruction on the FOG output signal to obtain a denoised gyro signal. According to the invention, in the event of denoising the FOG output signal by utilizing the OMDWT, the wavelet coefficient and the scale coefficient of the OMDWT circularly move for corresponding beats along with circular motion of the FOG signal; in the conversion process, the gyro signal is decomposed according to a plurality of channels; the FOG signal denoising method has rapider decomposition speed according to different bands, more detailed band division on the gyro signal and a denoising effect prior to the traditional wavelet denoising effect; and the FOG signal denoising method disclosed by the invention has a important meaning for increasing the navigation performance of an inertial navigation system.

Description

A kind of based on overlapping M the signal of fiber optical gyroscope denoising method with wavelet transform
Technical field
The present invention relates to a kind of signal of fiber optical gyroscope denoising method based on overlapping M band wavelet transform (Overlap M-band Discrete Wavelet Transform, OMDWT), belong to inertial navigation technology field.
Background technology
Optical fibre gyro is taking Sagnac effect as the novel all solid state gyroscope that basis grows up, and is subject to the great attention of countries in the world, has become the desirable inertia device in low-accuracy strapdown inertial navigation, guidance system in a new generation.A gordian technique in Methods of Strapdown Inertial Navigation System is how completely independently to realize fast initial alignment, independently determines fast initial orientation angle and the horizontal attitude angle of carrier.The principal element that affects alignment of orientation (seeking north) precision is gyroscopic drift, and effectively eliminating gyroscopic drift is the key of guarantor's bit alignment precision.
Optical fibre gyro drift can be divided into two types of systematicness drift and random drifts.Because random drift is small nonlinearity, becomes when slow, be subject to the impact of the uncertain factors such as external environment condition simultaneously, cannot set up its accurate system model, in inertial navigation system, can not be compensated by simple method, therefore random drift becomes the important indicator of weighing gyroscope precision.In order to improve initial alignment precision, must adopt effective signal processing method to gyroscope signal process, suppress these random drifts.At present the processing of gyro signal is had to two kinds of thoughts: (1) sets up Modelling of Random Drift of Gyroscopes model, use the methods such as Kalman filtering, Wiener filtering to compensate; (2) directly gyro output signal is carried out to denoising Processing.Common method has digital low-pass filtering, auto adapted filtering and wavelet threshold-value filter etc.In view of the characteristic of random drift, can not obtain in advance accurate statistical property, need to adopt direct filtering method to carry out denoising to gyro signal.
Small echo has good time-frequency resolution characteristic, is therefore applied in the denoising of signal of fiber optical gyroscope.In the existing analysis and research of the signal of fiber optical gyroscope based on wavelet theory, be all with small echo based on 2, denoising result has certain limitation, major embodiment is both ways: on the one hand, along with the carrying out of decomposing, the length of wavelet coefficient is successively decreased with 2 times of relations, and decomposition rate is slow; On the other hand, after the certain beat of signal of fiber optical gyroscope loopy moving, its wavelet transform (Discrete Wavelet Transform, DWT) wavelet coefficient and scale coefficient can not the same beats of loopy moving, and denoising effect is poor.
Summary of the invention
Technology of the present invention is dealt with problems and is: technology of the present invention is for the deficiency in existing signal of fiber optical gyroscope analytical approach, and overlapping M band wavelet transform is introduced to Gyro Sigal Denoising.On the one hand, overcome the signal of fiber optical gyroscope with small echo based on 2 and processed the slow deficiency of decomposition rate, what M was wavelet basis with wavelet theory chooses provides choice widely; Decomposing under sub band number the same terms, in M band wavelet transform (M-band Discrete Wavelet Transform, MDWT), signal decomposes by hyperchannel; On the other hand, overcome while carrying out signal of fiber optical gyroscope denoising based on 2 band small echos, after the certain beat of signal of fiber optical gyroscope loopy moving, the deficiency that DWT small echo and scale coefficient can not the same beats of loopy moving.
Technical solution of the present invention is: the present invention proposes a kind of based on overlapping M the signal of fiber optical gyroscope denoising method with wavelet transform, provided and calculated that effective signal of fiber optical gyroscope decomposes, threshold value is processed and restructing algorithm.Concrete steps are as follows:
(1) set up Optical Fiber Gyroscope model
Figure BDA0000121565070000021
Wherein, X tfor Optical Fiber Gyroscope; T=0 ..., N-1, N represents the length of Optical Fiber Gyroscope; ω iefor earth rotation angular speed, ω ie=7.27 × 10 -5rad/s;
Figure BDA0000121565070000022
for the geographic latitude of test point; ε tfor gyroscopic drift, gyroscopic drift forms by being often worth component, periodic component and white noise, that is:
ε t=ε ddsin(2πf d0)+W t
Wherein, ε dfor normal value component, in the short time, be approximately a constant; Ω dfor the amplitude of periodic component; f dfor the frequency of periodic component; θ 0for initial phase; W tfor zero-mean white Gaussian noise.Ω in formula dsin (2 π f d+ θ 0) and W ttwo random drift items that form optical fibre gyro output.
(2) Optical Fiber Gyroscope is made to OMDWT wavelet decomposition
The Optical Fiber Gyroscope X of the length N that step (1) is obtained tdo OMDWT conversion, the OMDWT wavelet coefficient and the scale coefficient that OMDWT are converted to the j yardstick obtaining are used respectively N n dimensional vector n
Figure BDA0000121565070000031
with
Figure BDA0000121565070000032
represent,
Figure BDA0000121565070000033
corresponding element
Figure BDA0000121565070000034
with
Figure BDA0000121565070000035
corresponding element
Figure BDA0000121565070000036
be respectively:
W ‾ ~ j , t i ≡ Σ l = 0 L j - 1 h ~ j , l i X t - l mod N , V ~ j , t ≡ Σ l = 0 L j - 1 g ~ j , l X t - l mod N
In formula, t=0 ..., N-1, N represents the length of signal of fiber optical gyroscope; L=1 ..., L, L=2M represents J 0the length of MDWT wave filter on yardstick, M represents small echo band number, i.e. M band small echo; I=1 ..., M-1; J=J 0, J 0+ 1 ..., J, J 0the initial gauges that represents wavelet transformation, J represents the termination yardstick of wavelet transformation;
Figure BDA0000121565070000039
with
Figure BDA00001215650700000310
be respectively i wavelet filter coefficient and the scaling filter coefficient of OMDWT on j yardstick; LmodN represents that l is to N remainder.
h ~ j , l i ≡ h j , l i / M j / 2 , g ~ j , l ≡ g j , l / M j / 2
In formula,
Figure BDA00001215650700000313
{ g j, lrepresent respectively i wavelet filter coefficient and the scaling filter coefficient of MDWT on j yardstick.M j/2represent the j/2 power of M; Wave filter on j yardstick
Figure BDA00001215650700000314
length be L j≡ (M j-1) (L-1)+1.
To signal of fiber optical gyroscope X tcarry out filtering by Periodic filter respectively, can utilize the scale coefficient vector of signal of fiber optical gyroscope on j-1 yardstick
Figure BDA00001215650700000315
calculate the wavelet coefficient vector of signal of fiber optical gyroscope on j yardstick
Figure BDA00001215650700000316
with scale coefficient vector
Figure BDA00001215650700000317
element.
Figure BDA00001215650700000318
with
Figure BDA00001215650700000319
corresponding element is used respectively with
Figure BDA00001215650700000321
represent:
W ‾ ~ j , t i Σ l = 0 L - 1 h ~ l i V ~ j - 1 , t - M j - 1 mod N , t = 0,1 , . . . , N - 1
V ~ j , t = Σ l = 0 L - 1 g ~ l V ~ j - 1 , t - M j - 1 mod N , t = 0,1 , . . . , N - 1
In formula,
Figure BDA00001215650700000324
with
Figure BDA00001215650700000325
represent respectively i wavelet filter coefficient and the scaling filter coefficient of OMDWT;
Figure BDA00001215650700000326
represent t-M j-1the scale coefficient of lmodN moment j-1 yardstick, j=J 0, J 0+ 1 ..., J.
In above-mentioned conversion, OMDWT wavelet filter coefficient with scaling filter coefficient
Figure BDA0000121565070000042
solve as follows:
h ~ l i ≡ h l i / M , g ~ l ≡ g l / M
In formula, l=1 ..., L;
Figure BDA0000121565070000045
{ g lbe respectively i wavelet filter and the scaling filter coefficient of MDWT.
When step (2) is made OMDWT wavelet decomposition to signal of fiber optical gyroscope, thereby decompose speed by different frequency bands, and signal of fiber optical gyroscope is had to thinner frequency band division; After signal of fiber optical gyroscope loopy moving, its OMDWT wavelet coefficient and scale coefficient are understood the corresponding beat of loopy moving, are conducive to the signal denoising of optical fibre gyro.
(3) OMDWT wavelet coefficient is done to threshold value processing
The wavelet coefficient obtaining after signal of fiber optical gyroscope in step (2) is decomposed
Figure BDA0000121565070000046
do threshold value processing.Utilize threshold value processing, absolute value is less than to the wavelet coefficient zero setting of threshold value, but the wavelet coefficient that absolute value is greater than threshold value has been done to contraction.
W ~ j , t i ( W &OverBar; ~ j , t i , T s ) = W &OverBar; ~ j , t i - T s , W &OverBar; ~ j , t i &GreaterEqual; T s 0 | W &OverBar; ~ j , t i | < T s W &OverBar; ~ j , t i + T s W &OverBar; ~ j , t i &le; - T s
In formula, T sthreshold value, 10 -5< T s< 10 -3;
Figure BDA0000121565070000048
be illustrated in yardstick j upper through threshold value i wavelet coefficient after treatment.
(4) Optical Fiber Gyroscope after thresholding threshold process is carried out to OMDWT wavelet reconstruction
V ~ j - 1 , t = &Sigma; l = 0 L - 1 &Sigma; i = 1 M - 1 h ~ l i W ~ j , t + M j - 1 l mod N i + &Sigma; l = 0 L - 1 g ~ l V ~ j , t + M j - 1 l mod N
In formula,
Figure BDA00001215650700000410
represent the scale coefficient of t moment j-1 yardstick; with
Figure BDA00001215650700000412
represent respectively t+M j-1the scale coefficient of scale j and threshold value i wavelet coefficient after treatment when lmodN.
Utilize above formula through calculating, finally at J 0on yardstick, obtain the signal of fiber optical gyroscope after the denoising of reconstruct X ~ = V ~ J 0 , t .
The present invention's advantage is compared with prior art: the present invention in the time carrying out denoising, thereby decompose speed by different frequency bands, and signal of fiber optical gyroscope is had to thinner frequency band division; (2) after signal of fiber optical gyroscope loopy moving, its OMDWT wavelet coefficient and scale coefficient are understood the corresponding beat of loopy moving, are conducive to the signal denoising of optical fibre gyro.
Brief description of the drawings
Fig. 1 is calculation flow chart of the present invention.
Embodiment
As shown in Figure 1, implementation method of the present invention is as follows:
1, set up Optical Fiber Gyroscope model
Figure BDA0000121565070000051
Wherein, X tfor Optical Fiber Gyroscope; T=0 ..., N-1, N represents the length of Optical Fiber Gyroscope; ω iefor earth rotation angular speed, ω ie=7.27 × 10 -5rad/s;
Figure BDA0000121565070000052
for the geographic latitude of test point; ε tfor gyroscopic drift, gyroscopic drift forms by being often worth component, periodic component and white noise,
ε t=ε ddsin(2πf d0)+W t (2)
In formula, ε dfor normal value component, in the short time, be approximately a constant; Ω dfor the amplitude of periodic component; f dfor the frequency of periodic component; θ 0for initial phase; W tfor zero-mean white Gaussian noise.Ω in formula dsin (2 π f d+ θ 0) and W ttwo random drift items that form optical fibre gyro output.
2, Optical Fiber Gyroscope is made to OMDWT wavelet decomposition
A. Optical Fiber Gyroscope being made to OMDWT mono-step decomposes
Order
Figure BDA0000121565070000053
Figure BDA0000121565070000054
X t = X 0 X 1 . . . X N - 3 X N - 2 X N - 1
Definition
Figure BDA0000121565070000061
One step decomposable process of OMDWT algorithm is: use wavelet coefficient
Figure BDA0000121565070000063
respectively to X t,
Figure BDA0000121565070000064
Figure BDA0000121565070000065
carry out MDWT decomposition, obtain
Figure BDA0000121565070000066
and V 1, and arrange by formula (5).That is to say, carry out, after M MDWT decomposition, M group coefficient being lined up,
Figure BDA0000121565070000067
Wherein,
Figure BDA0000121565070000068
in subscript i represent that this matrix is made up of with i wavelet coefficient of wavelet transformation M.
Figure BDA0000121565070000069
For example, work as M=3, when L=6
Figure BDA00001215650700000610
Wavelet filter coefficient in wushu (6) replace with g l, obtain
Figure BDA00001215650700000612
Figure BDA00001215650700000613
and V 1element can be expressed as:
W 1 i = [ M 1 / M W ~ 1 , M - 1 i , M 1 / M W ~ 1,2 M - 1 i , M 1 / M W ~ 1,3 M - 1 i , . . . , M 1 / M W ~ 1 , N - 1 i ] T - - - ( 8 )
V 1 = [ M 1 / M V ~ 1 , M - 1 , M 1 / M V ~ 1,2 M - 1 , M 1 / M V ~ 1,3 M - 1 , . . . , M 1 / M V ~ 1 , N - 1 ] T - - - ( 9 )
Can find out, use wavelet filter
Figure BDA0000121565070000071
and scaling filter { g land time series X tcyclic convolution, obtains
Figure BDA0000121565070000072
and V 1.
Figure BDA0000121565070000073
and V 1the sequence that is N by length respectively
Figure BDA0000121565070000074
with
Figure BDA0000121565070000075
m-1,2M-1 ..., N-1 element composition.
X in wushu (5) treplace with loopy moving vector
Figure BDA0000121565070000076
with
Figure BDA0000121565070000077
have
Figure BDA0000121565070000078
Figure BDA0000121565070000079
Figure BDA00001215650700000710
Definition
Figure BDA00001215650700000711
Figure BDA00001215650700000712
Figure BDA00001215650700000713
Figure BDA00001215650700000714
Figure BDA00001215650700000716
For example, work as M=3, when L=6, have
Figure BDA0000121565070000081
Figure BDA0000121565070000082
Figure BDA0000121565070000083
replace with g l, can obtain
Figure BDA0000121565070000084
with
Figure BDA0000121565070000085
Figure BDA0000121565070000086
element can be expressed as:
Figure BDA0000121565070000087
Figure BDA0000121565070000088
element can be expressed as:
Equally,
Figure BDA00001215650700000810
element can be expressed as:
Figure BDA00001215650700000811
Figure BDA00001215650700000812
element can be expressed as:
Figure BDA00001215650700000813
Definition
W ~ 1 i &equiv; [ W ~ 1,0 i , W ~ 1,1 i , W ~ 1,2 i , . . . , W ~ 1 , N - 1 i ] T - - - ( 21 )
V ~ 1 &equiv; [ V ~ 1,0 , V ~ 1,1 , V ~ 1,2 , . . . , V ~ 1 , N - 1 ] T - - - ( 22 )
Will with
Figure BDA00001215650700000817
element divided by coefficient M 1/M, and they are arranged by formula (21), can obtain by similar approach by V 1,
Figure BDA00001215650700000819
with
Figure BDA00001215650700000820
obtain.Here,
Figure BDA00001215650700000821
with
Figure BDA00001215650700000822
element be actually the wave filter with OMDWT
Figure BDA00001215650700000823
with
Figure BDA00001215650700000824
to X tafter filtering, the output obtaining
Figure BDA00001215650700000825
with
Figure BDA00001215650700000826
by matrix
Figure BDA00001215650700000827
with
Figure BDA00001215650700000828
in each
Figure BDA00001215650700000829
replace with
Figure BDA00001215650700000830
and the row in these matrixes is arranged by formula (23), obtain N × N matrix
Figure BDA0000121565070000091
Figure BDA0000121565070000092
For example, work as M=3, when L=6
Therefore
Figure BDA0000121565070000094
In wushu (23) replace with
Figure BDA0000121565070000096
can obtain
Figure BDA0000121565070000097
Figure BDA0000121565070000098
finally, a step exploded representation of OMDWT algorithm be:
Figure BDA0000121565070000099
wherein
Figure BDA00001215650700000910
By this process, when signal of fiber optical gyroscope is made to OMDWT wavelet decomposition, thereby decompose speed by different frequency bands, and signal of fiber optical gyroscope is had to thinner frequency band division; After signal of fiber optical gyroscope loopy moving, its OMDWT wavelet coefficient and scale coefficient can the corresponding beats of loopy moving.
B. ask signal of fiber optical gyroscope X toMDWT conversion on j yardstick
The signal of fiber optical gyroscope X of the length N that step 1 is obtained tdo OMDWT conversion, the OMDWT wavelet coefficient of j yardstick and scale coefficient are used respectively to N n dimensional vector n
Figure BDA0000121565070000101
with
Figure BDA0000121565070000102
represent,
Figure BDA0000121565070000103
corresponding element
Figure BDA0000121565070000104
with
Figure BDA0000121565070000105
corresponding element
Figure BDA0000121565070000106
be respectively:
W &OverBar; ~ j , t i &equiv; &Sigma; l = 0 L j - 1 h ~ j , l i X t - l mod N , V ~ j , t &equiv; &Sigma; l = 0 L j - 1 g ~ j , l X t - l mod N , i = 1 , . . . , M - 1 - - - ( 27 )
In formula, t=0 ..., N-1, N represents the length of signal of fiber optical gyroscope; L=1 ..., L, j=J 0, J 0+ 1 ..., J, J 0the initial gauges that represents wavelet transformation, J represents the termination yardstick of wavelet transformation; with
Figure BDA00001215650700001010
be respectively i wavelet filter coefficient and the scaling filter coefficient of OMDWT on j yardstick; LmodN represents that l is to N remainder.
h ~ j , l i &equiv; h j , l i / M j / 2 , g ~ j , l &equiv; g j , l / M j / 2 - - - ( 28 )
Figure BDA00001215650700001013
{ g j, lrepresent respectively i wavelet filter coefficient and the scaling filter coefficient of MDWT on j yardstick.Can push away, wave filter
Figure BDA00001215650700001014
length be L j≡ (M j-1) (L-1)+1.
Utilize the scale coefficient vector of signal of fiber optical gyroscope on j-1 yardstick
Figure BDA00001215650700001015
calculate the wavelet coefficient vector of signal of fiber optical gyroscope on j yardstick
Figure BDA00001215650700001016
with scale coefficient vector
Figure BDA00001215650700001017
element.
Figure BDA00001215650700001018
with
Figure BDA00001215650700001019
corresponding element is used respectively
Figure BDA00001215650700001020
with
Figure BDA00001215650700001021
represent:
W &OverBar; ~ j , t i &Sigma; l = 0 L - 1 h ~ l i V ~ j - 1 , t - M j - 1 mod N , t = 0,1 , . . . , N - 1 - - - ( 29 )
V ~ j , t = &Sigma; l = 0 L - 1 g ~ l V ~ j - 1 , t - M j - 1 mod N , t = 0,1 , . . . , N - 1 - - - ( 30 )
In formula,
Figure BDA00001215650700001024
with
Figure BDA00001215650700001025
represent respectively i wavelet filter coefficient and the scaling filter coefficient of OMDWT; represent t-M j-1the scale coefficient of lmodN moment j-1 yardstick, j=J 0, J 0+ 1 ..., J.
C. ask OMDWT wavelet filter coefficient
Figure BDA0000121565070000111
with scaling filter coefficient
h ~ l i &equiv; h l i / M , g ~ l &equiv; g l / M - - - ( 31 )
In formula, l=1 ..., L; I=1 ..., M-1;
Figure BDA0000121565070000115
{ g lbe respectively i wavelet filter and the scaling filter coefficient of MDWT.
3, OMDWT wavelet coefficient is done to threshold value processing
The wavelet coefficient obtaining after signal of fiber optical gyroscope in step 2 is decomposed
Figure BDA0000121565070000116
do threshold value processing.Utilize threshold value processing, absolute value is less than to the wavelet coefficient zero setting of threshold value, but the wavelet coefficient that absolute value is greater than threshold value has been done to contraction.
W ~ j , t i ( W &OverBar; ~ j , t i , T s ) = W &OverBar; ~ j , t i - T s , W &OverBar; ~ j , t i &GreaterEqual; T s 0 | W &OverBar; ~ j , t i | < T s W &OverBar; ~ j , t i + T s W &OverBar; ~ j , t i &le; - T s , t = 0,1 , . . . , N - 1 - - - ( 32 )
In formula, T sthreshold value, 10 -5< T s< 10 -3;
Figure BDA0000121565070000118
be illustrated in yardstick j upper through threshold value i wavelet coefficient after treatment.
4, the OMDWT restructing algorithm following formula that the Optical Fiber Gyroscope after thresholding threshold process is carried out to OMDWT wavelet reconstruction Optical Fiber Gyroscope is described:
V ~ j - 1 , t i = &Sigma; l = 0 L - 1 &Sigma; i = 1 M - 1 h ~ l i W ~ j , t + M j - 1 l mod N i + &Sigma; l = 0 L - 1 g ~ l V ~ j , t + M j - 1 l mod N - - - ( 33 )
In formula, t=0,1 ..., N-1;
Figure BDA00001215650700001110
with represent respectively t+M j-1the scale coefficient of scale j and threshold value i wavelet coefficient after treatment when lmodN.
Utilize above formula through calculating, finally at J 0on yardstick, obtain the signal of fiber optical gyroscope after the denoising of reconstruct X ~ = V ~ J 0 , t .
The present invention is based on OMDWT signal of fiber optical gyroscope is carried out to denoising, compared with the signal of fiber optical gyroscope denoising method with small echo based on 2, computing velocity is fast, and noise ratio of compression is large.
The content not being described in detail in instructions of the present invention belongs to the known prior art of professional and technical personnel in the field.

Claims (3)

1. the signal of fiber optical gyroscope denoising method with wavelet transform based on overlapping M, is characterized in that performing step is as follows:
(1) set up Optical Fiber Gyroscope model
Figure FDA0000426626110000011
Wherein, X tfor Optical Fiber Gyroscope; T=0 ..., N-1, N represents the length of Optical Fiber Gyroscope; ω iefor earth rotation angular speed, ω ie=7.27 × 10 -5rad/s;
Figure FDA0000426626110000012
for the geographic latitude of test point; ε tfor gyroscopic drift;
(2) Optical Fiber Gyroscope is made to OMDWT wavelet decomposition
First, use with
Figure FDA0000426626110000014
respectively to Optical Fiber Gyroscope X tcarry out filtering, obtain J 0wavelet coefficient on yardstick and scale coefficient; Then, obtained scale coefficient is used with carry out filtering, obtain wavelet coefficient and the scale coefficient of OMDWT on j yardstick, the OMDWT wavelet coefficient of the j yardstick obtaining and scale coefficient are used respectively to N n dimensional vector n
Figure FDA0000426626110000017
with
Figure FDA0000426626110000018
represent,
Figure FDA0000426626110000019
corresponding element
Figure FDA00004266261100000110
with corresponding element
Figure FDA00004266261100000112
be respectively:
W ~ &OverBar; j , t i &equiv; &Sigma; l = 0 L j - 1 h ~ j , l i X t - l mod N , V ~ j , t &equiv; &Sigma; l = 0 L j - 1 g ~ j , l X t - l mod N ;
In formula, t=0 ..., N-1, N represents the length of signal of fiber optical gyroscope; L=1 ..., L, L=2M represents J 0the length of MDWT wave filter on yardstick, M represents small echo band number, i.e. M band small echo; I=1 ..., M-1; J=J 0, J 0+ 1 ..., J, J 0the initial gauges that represents wavelet transformation, J represents the termination yardstick of wavelet transformation; LmodN represents that l is to N remainder;
Calculate successively, to yardstick J,
Wherein, with be respectively J 0i wavelet filter coefficient of OMDWT and scaling filter coefficient on yardstick,
Figure FDA00004266261100000116
with
Figure FDA00004266261100000117
be respectively i wavelet filter coefficient and the scaling filter coefficient of OMDWT on j yardstick;
h ~ j , l i &equiv; h j , l i / M j / 2 , g ~ j , l &equiv; g j , l / M j / 2 - - - ( 2 )
In formula,
Figure FDA0000426626110000022
with
Figure FDA0000426626110000023
represent respectively i wavelet filter coefficient and the scaling filter coefficient of MDWT on j yardstick; M j/2represent the j/2 power of M; Wave filter on j yardstick
Figure FDA0000426626110000024
length be L j≡ (M j-1) (L-1)+1;
(3) OMDWT wavelet coefficient is done to threshold value processing
The wavelet coefficient obtaining after signal of fiber optical gyroscope in step (2) is decomposed
Figure FDA0000426626110000025
do threshold value processing, utilize threshold value processing, absolute value is less than to the wavelet coefficient zero setting of threshold value, but the wavelet coefficient that absolute value is greater than threshold value has been done to contraction:
W ~ j , t i ( W ~ &OverBar; j , t i , T s ) = W ~ &OverBar; j , t i - T s , W ~ &OverBar; j , t i &GreaterEqual; T s 0 | W ~ &OverBar; j , t i | < T s W ~ &OverBar; j , t i + T s , W ~ &OverBar; j , t i &le; - T s - - - ( 3 )
In formula, t=0,1 ..., N-1, T sit is threshold value;
Figure FDA0000426626110000027
be illustrated in yardstick j upper through threshold value i wavelet coefficient after treatment;
(4) Optical Fiber Gyroscope after thresholding threshold process is carried out to OMDWT wavelet reconstruction:
V ~ j - 1 , t = &Sigma; l = 0 L - 1 &Sigma; i = 1 M - 1 h ~ l i W ~ j , t + M j - 1 l mod N i + &Sigma; l = 0 L - 1 g ~ l V ~ j , t + M j - 1 l mod N - - - ( 4 )
In formula, j=J 0, J 0+ 1 ..., J; L=1 ..., L, L=2M represents J 0the length of MDWT wave filter on yardstick, M represents small echo band number, i.e. M band small echo;
Figure FDA0000426626110000029
with
Figure FDA00004266261100000210
represent respectively i wavelet filter coefficient and the scaling filter coefficient of OMDWT;
Figure FDA00004266261100000211
represent the scale coefficient of t moment j-1 yardstick;
Figure FDA00004266261100000212
with
Figure FDA00004266261100000213
represent respectively t+M j-1i wavelet coefficient when lmodN after scale j Upper threshold threshold process and scale coefficient;
(5) utilize formula (4) through calculating, finally at J 0on yardstick, obtain the signal of fiber optical gyroscope after the denoising of reconstruct
According to claim 1 a kind of based on overlapping M the signal of fiber optical gyroscope denoising method with wavelet transform, it is characterized in that: when described step (2) is made OMDWT wavelet decomposition to signal of fiber optical gyroscope, obtain the scale coefficient of OMDWT on j yardstick
Figure FDA0000426626110000031
and wavelet coefficient
Figure FDA0000426626110000032
implementation procedure as follows:
Figure FDA0000426626110000033
wherein
Wherein:
Figure FDA0000426626110000035
Figure FDA0000426626110000036
In wushu (7)
Figure FDA0000426626110000037
replace with
Figure FDA0000426626110000038
obtain
Figure FDA0000426626110000039
Figure FDA00004266261100000310
with
Figure FDA00004266261100000311
be respectively i wavelet filter coefficient and the scaling filter coefficient of OMDWT.
According to claim 1 based on overlapping M the signal of fiber optical gyroscope denoising method with wavelet transform, it is characterized in that: described T svalue is 10 -5< T s< 10 -3.
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