CN103954392A - Device for measuring torsional pendulum micro impulse through linear frequency modulation multi-beam laser heterodyning and torsional pendulum micro impulse measuring method based on device - Google Patents

Abstract

The invention provides a device for measuring torsional pendulum micro impulse through linear frequency modulation multi-beam laser heterodyning and a torsional pendulum micro impulse measuring method based on the device, and belongs to the field of torsional pendulum micro impulse measurement. The device and method are used for solving the problem that an existing torsional pendulum micro impulse measurement method and device are low in measurement precision. Laser emitted by a pulse laser acts on a working medium target to generate plasma jet, the back jet effect enables a standard beam to rotate, while the standard beam rotates, a linear frequency modulation laser continuously emits linear frequency modulation laser light which is reflected to a plane standard mirror through a first plane mirror and a second plane mirror, the front surface and the rear surface of the plane standard mirror both reflect the linear frequency modulation laser light, the linear frequency modulation laser light is gathered on the photosensitive face of a photoelectric detector through a convergent lens, the photoelectric detector sends electric signals to a signal processing system to obtain a tilt angle theta' of the standard beam, and according to a formula, micro impulse I' generated by the effect of the laser emitted by the pulse laser and the working medium target is obtained. The device and method are suitable for measuring the torsional pendulum micro impulse.

Description

The measurement of linear frequency modulation multi-beam laser heterodyne is rocked the device of micro-momentum and based on the micro-impulse measurement method of rocking of this device

Technical field

The present invention relates to rock micro-impulse measurement technical field.

Background technology

Laser microthruster has extensive and deep application prospect at microsatellite attitude and track control field, it has than leaping high, large, the minimum momentum of momentum dynamic range is little, low in energy consumption, Energy Coupling efficiency is high and be easy to the significant advantages such as realization, lightweight and Digital Control, has been subject to Chinese scholars and has paid close attention to widely.And momentum is an important parameter of reflection laser microthruster performance, feature is that magnitude is little, is about 10 ^-7～10 ^-5ns.The people such as the Photonic Associates Phipps of group have proposed the micro impulse producing with rocking systematic survey laser microthruster in 1999, and carry out the test of microthruster performance parameter with it; 2002, the people such as Phipps improved the system of rocking again, and domestic Chinese University of Science and Technology and equipment Command technical college have also carried out correlative study subsequently.From the result of study of reporting both at home and abroad at present, on the one hand, the noise of measuring system can affect the precision of system, and in little momentum magnitude, systematic error has even reached 50%; Meanwhile, within power action time, target plane departs from focal plane, Energy Coupling Efficiency Decreasing, and this also can affect the measurement of micro-momentum, and therefore conventional little impulse measurement system is difficult to meet and measures requirement.

Laser interferance method can effectively solve above two problems that conventionally test system exists, and improves the measuring accuracy of system.The method that adopts two corner cubes to form variate replaces original light pointer method measurement to rock the angle of rotation, has greatly improved the precision of system; Rock the Push Technology quality of 2010 and be increased to 58g by original 0.2g, overcome out of focus problem.Result of study shows, the introducing of laser interferance method has greatly improved the performance of rocking test macro, can meet the test request of laser microthruster micro impulse.But because measuring amount is more indirectly, accidental error is larger, and therefore measuring accuracy can be very not high yet.

Summary of the invention

The present invention is for the low problem of measuring accuracy of the apparatus and method that solve existing measurement and rock micro-momentum, proposed that the device of micro-momentum is rocked in the measurement of linear frequency modulation multi-beam laser heterodyne and based on the micro-impulse measurement method of rocking of this device.

The device that micro-momentum is rocked in the measurement of property frequency modulation multi-beam laser heterodyne comprises linear frequency modulation laser instrument, the first plane mirror, the second plane mirror, plane standard mirror, Standard Beam, vacuum chamber, pulsed laser, working medium target, convergent lens, photodetector and signal processing system

Described linear frequency modulation laser instrument, the first plane mirror, the second plane mirror, plane standard mirror, Standard Beam, pulsed laser, working medium target and convergent lens are all placed in vacuum chamber,

The center of described Standard Beam is fixed with turning axle,

Described working medium target is pasted the upper surface at Standard Beam, and the second plane mirror is pasted the lower surface at Standard Beam, and working medium target and the second plane mirror be all positioned at same one end of Standard Beam,

The laser action that pulse laser is launched produces plasma spraying in working medium target, the effect of regurgitating rotates Standard Beam, when Standard Beam rotates, linear frequency modulation laser instrument continues to launch linear frequency modulation laser, linear frequency modulation laser is incident to plane standard mirror after the first plane mirror and the reflection of the second plane mirror, the front surface of plane standard mirror and rear surface are all reflected linear frequency modulation laser and are converged to by convergent lens on the photosurface of photodetector, the electrical signal of photodetector is connected with the electric signal input end of signal processing system.

Described signal processing system comprises wave filter, prime amplifier, A/D converter and DSP, the electric signal input end of wave filter is connected as the electric signal input end of signal processing system and the electrical signal of photodetector, the filtering signal output terminal of wave filter is connected with the filtering signal input end of prime amplifier, the amplifying signal output terminal of prime amplifier is connected with the input end of analog signal of A/D converter, and the digital signal output end of A/D converter is connected with the digital signal input end of DSP.

On described vacuum chamber, have vacuum window, described vacuum window is for making the light in vacuum chamber assemble the photodetector photosurface to vacuum chamber outside.

Based on described linear frequency modulation multi-beam laser heterodyne measurement rock micro-momentum device rock micro-impulse measurement method by following process implementation:

Pulsed laser, linear frequency modulation laser instrument, photodetector and signal processing system are switched to duty, photodetector is converted to electric signal by the light signal receiving and is sent to signal processing system, signal processing system obtains the pivot angle θ ' of Standard Beam according to the continuous electric signal receiving

According to:

$I^{\′}=\frac{2\mathrm{J\ω}}{D}\·{\mathrm{\θ}}^{\′}=\frac{4\mathrm{\πJ}}{{\mathrm{DT}}^{\′}}\·{\mathrm{\θ}}^{\′}$ (formula one),

Micro-momentum I ' that the laser that acquisition pulsed laser sends and the effect of working medium target produce, wherein, J is the moment of inertia of the system of rocking, and ω is damped frequency, and T ' is damping period, and D is Standard Beam length, makes k=4 π J/DT ':

I '=k θ ' (formula two).

Signal processing system obtains Standard Beam pivot angle θ ' according to the continuous electric signal receiving is by following process implementation:

When the lasting linear frequency modulation laser of launching of linear frequency modulation laser instrument is with incidence angle θ ₀oblique incidence is during to plane standard mirror, and the incident field E (t) of plane standard mirror is:

E (t)=E ₀exp{i (ω ₀t+k ' t ²) (formula three),

Wherein, for the rate of change of modulating bandwidth, T is the frequency modulation cycle, and △ F is modulating bandwidth, E ₀for incident field amplitude, t is the time, ω ₀for incident field angular frequency, i represents imaginary number,

If it is l that linear frequency modulation laser arrives the light path of plane standard mirror front surface, linear laser of frequency modulation of t-l/c moment arrives the reflection light field E of plane standard mirror front surface ₁(t) be:

$E_1\left(t\right)={\mathrm{\α}}_1{E}_0\exp \left\{i\right[{\mathrm{\ω}}_0(t-\frac{l}{c})+k^{\′}{(t-\frac{l}{c})}^2\left]\right\}$ (formula four),

The light of plane standard mirror front surface transmission is not all being carried out multiple reflections and refraction by the front surface of plane standard mirror and rear surface in the same time, and the catoptrical light field that reflection obtains is each time:

$\left\{\begin{array}{c}{E}_2\left(t\right)={\mathrm{\α}}_2{E}_0\exp \left\{i\right[{\mathrm{\ω}}_0(t-\frac{l+2\mathrm{nd}\cos \mathrm{\θ}}{c})+k^{\′}{(t-2\mathrm{nd}\cos \mathrm{\θ})}^2+\frac{2{\mathrm{\ω}}_0\mathrm{nd}\cos \mathrm{\θ}}{c}\left]\right\}\\ E_3\left(t\right)={\mathrm{\α}}_3{E}_0\exp \left\{i\right[{\mathrm{\ω}}_0(t-\frac{l+4\mathrm{nd}\cos \mathrm{\θ}}{c})+k^{\′}{(t-\frac{l+4\mathrm{nd}\cos \mathrm{\θ}}{c})}^2+\frac{4{\mathrm{\ω}}_0\mathrm{nd}\cos \mathrm{\θ}}{c}\left]\right\}\\ .\\ .\\ .\\ E_m=\left(t\right)={\mathrm{\α}}_m{E}_0\exp \left\{i\right[{\mathrm{\ω}}_0(t-\frac{l+2(m-1)\mathrm{nd}\cos \mathrm{\θ}}{c})+k^{\′}{(t-\frac{l+2(m-1)\mathrm{nd}\cos \mathrm{\θ}}{c})}^2+\frac{2(m-1){\mathrm{\ω}}_0\mathrm{nd}\cos \mathrm{\θ}}{c}\left]\right\}\\ .\\ .\\ .\end{array}\right.$

(formula five),

Wherein, m is nonnegative integer, α ₁=r, α _m=β β ' r ' ^(2m-3)(m>=2), r is the reflectivity of light while injecting plane standard mirror from surrounding medium, β is the transmissivity of light while injecting plane standard mirror from surrounding medium, r ' is the reflectivity of plane standard mirror rear surface, transmissivity when β ' is injected into surrounding medium for light from plane standard mirror inside, and d is plane standard mirror thickness, θ is refraction angle, n is plane standard mirror refractive index, and c is the light velocity

Total light field E ' that photodetector receives is (t):

E ' (t)=E ₁(t)+E ₂(t)+...+E _m(t)+... (formula six),

The photocurrent I of photodetector output is:

$I=\frac{\mathrm{\ηe}}{\mathrm{hv}}\frac{1}{Z}\underset{D}{\∫\∫}\frac{1}{2}[E_1\left(t\right)+E_2\left(t\right)+...+E_m\left(t\right)+...]{[E_1\left(t\right)+E_2\left(t\right)+...+E_m\left(t\right)+...]}^{*}\mathrm{ds}$ (formula seven),

Wherein, e is electron charge, and Z is the intrinsic impedance of photodetector surfaces medium, and η is quantum efficiency, and D is the area of photodetector photosurface, and h is Planck's constant, and v is laser frequency, represents complex conjugate No. *,

Obtain electric current of intermediate frequency I according to formula seven _iFfor:

$I_{\mathrm{IF}}=\frac{\mathrm{\ηe}}{2\mathrm{hv}}\frac{1}{Z}\underset{D}{\∫\∫}\underset{p=0}{\overset{m-1}{\mathrm{\Σ}}}\underset{j=0}{\overset{m-p}{\mathrm{\Σ}}}(E_j\left(t\right){E_{j+p}}^{*}\left(t\right)+{E_j}^{*}\left(t\right)E_{j+p}\left(t\right))\mathrm{ds}$ (formula eight),

By in formula four and formula five substitution formula eight, arrange:

$I_{\mathrm{IF}}=\frac{\mathrm{\ηe}}{\mathrm{hv}}\frac{\mathrm{\π}}{Z}{E}_0^2\underset{p=0}{\overset{m-1}{\mathrm{\Σ}}}\underset{j=0}{\overset{m-p}{\mathrm{\Σ}}}{\mathrm{\α}}_{j+p}{\mathrm{\α}}_j\cos (\frac{4p{k}^{\′}\mathrm{nd}\cos \mathrm{\θ}}{c}t-\frac{4p{k}^{\′}\mathrm{nd}\cos \mathrm{\θ}(l+\mathrm{nd}\cos \mathrm{\θ})}{c^2})$ (formula nine),

Intermediate frequency item difference on the frequency in formula nine is carried out to Fourier transform, obtain the frequency f of interference signal _pfor:

$f_p=\frac{2{\mathrm{pk}}^{\′}\mathrm{nd}\cos \mathrm{\θ}}{\mathrm{\πc}}=K_p\cos \mathrm{\θ}$ (formula ten),

Thereby obtain the value of refraction angle θ, wherein K _pfor scale-up factor, and

According to the known refraction angle θ of refraction law and incidence angle θ ₀pass be:

θ ₀=arcsin (nsin θ) (formula 11),

According to the known incidence angle θ of input path geometric relationship ₀with the pass of the pivot angle θ ' of Standard Beam (3) be:

${\mathrm{\θ}}^{\′}=\frac{{\mathrm{\θ}}_0}{2}=\frac{\arcsin \left(n\sin \mathrm{\θ}\right)}{2}$ (formula 12),

By in the value substitution formula two of the pivot angle θ ' of the Standard Beam obtaining in formula 12, micro-momentum I' that the laser that acquisition pulsed laser sends and the effect of working medium target produce.

Beneficial effect: what the present invention proposed rocks that micro-impulse measurement method range of linearity is large, resolution is high, the advantage of this angle-measuring method is to rotation sensitive, insensitive to translation, therefore device of the present invention also has compared with strong anti-interference ability vibration, particularly low-frequency vibration, can within several seconds, return to working state of system, not only reduce measuring error, also reduce the requirement to measuring equipment and bad border of experiment.Simultaneously, when rotational angle less (being less than 5 °), momentum and the incident angle surveyed are linear, and measuring error is less than 0.48%, can meet the requirement of laser microthruster impulse measurement, for the performance of assessment laser microthruster provides good measurement means.

Brief description of the drawings

Fig. 1 is the structural representation that the device of micro-momentum is rocked in the linear frequency modulation multi-beam laser heterodyne measurement described in embodiment one and embodiment two;

Fig. 2 is the linear frequency modulation multi-beam laser principle of interference schematic diagram of plane standard mirror;

Fig. 3 is spectrogram corresponding to micro-impulse measurement in different incidence angles situation.

Embodiment

Embodiment one, in conjunction with Fig. 1, this embodiment is described, the device that micro-momentum is rocked in linear frequency modulation multi-beam laser heterodyne measurement described in this embodiment comprises linear frequency modulation laser instrument 5, the first plane mirror 6, the second plane mirror 4, plane standard mirror 7, Standard Beam 3, vacuum chamber 11, pulsed laser 1, working medium target 2, convergent lens 8, photodetector 9 and signal processing system 10

Described linear frequency modulation laser instrument 5, the first plane mirror 6, the second plane mirror 4, plane standard mirror 7, Standard Beam 3, pulsed laser 1, working medium target 2 and convergent lens 8 are all placed in vacuum chamber 11,

The center of described Standard Beam 3 is fixed with turning axle,

Described working medium target 2 is pasted the upper surface at Standard Beam 3, and the second plane mirror 4 is pasted the lower surface at Standard Beam 3, and working medium target 2 and the second plane mirror 4 be all positioned at same one end of Standard Beam 3,

The laser action that pulse laser is launched produces plasma spraying in working medium target 2, the effect of regurgitating rotates Standard Beam 3, when Standard Beam 3 rotates, linear frequency modulation laser instrument 5 continues to launch linear frequency modulation laser, linear frequency modulation laser is incident to plane standard mirror 7 after the first plane mirror 6 and the second plane mirror 4 reflections, the front surface of plane standard mirror 7 and rear surface are all reflected linear frequency modulation laser and are converged to by convergent lens 8 on the photosurface of photodetector 9, the electrical signal of photodetector 9 is connected with the electric signal input end of signal processing system 10.

Embodiment two, in conjunction with Fig. 1, this embodiment is described, this embodiment is with the difference that the device of micro-momentum is rocked in the linear frequency modulation multi-beam laser heterodyne measurement described in embodiment one, described signal processing system 10 comprises wave filter 10-1, prime amplifier 10-2, A/D converter 10-3 and DSP10-4, the electric signal input end of wave filter 10-1 is connected with the electrical signal of photodetector 9 as the electric signal input end of signal processing system 10, the filtering signal output terminal of wave filter 10-1 is connected with the filtering signal input end of prime amplifier 10-2, the amplifying signal output terminal of prime amplifier 10-2 is connected with the input end of analog signal of A/D converter 10-3, the digital signal output end of A/D converter 10-3 is connected with the digital signal input end of DSP10-4.

Embodiment three, in conjunction with Fig. 1, this embodiment is described, the difference that the device of micro-momentum is rocked in linear frequency modulation multi-beam laser heterodyne measurements described in this embodiment and embodiment one is, described vacuum window is used for making the light in vacuum chamber 11 assemble photodetector 9 photosurfaces to vacuum chamber 11 outsides.

Embodiment four, linear frequency modulation multi-beam laser heterodyne measurement based on described in embodiment a gang of embodiment two rock micro-momentum device rock micro-impulse measurement method by following process implementation:

Pulsed laser 1, linear frequency modulation laser instrument 5, photodetector 9 and signal processing system 10 are switched to duty, photodetector 9 is converted to electric signal by the light signal receiving and is sent to signal processing system 10, signal processing system 10 obtains the pivot angle θ ' of Standard Beam 3 according to the continuous electric signal receiving

According to:

$I^{\′}=\frac{2\mathrm{J\ω}}{D}\·{\mathrm{\θ}}^{\′}=\frac{4\mathrm{\πJ}}{{\mathrm{DT}}^{\′}}\·{\mathrm{\θ}}^{\′}$ (formula one),

Micro-momentum I ' that the laser that acquisition pulsed laser 1 sends and the effect of working medium target produce, wherein, J is the moment of inertia of the system of rocking, and ω is damped frequency, and T ' is damping period, and D is Standard Beam 3 length, makes k=4 π J/DT ':

I '=k θ ' (formula two).

Embodiment five, in conjunction with Fig. 2, this embodiment is described, the difference of rocking micro-impulse measurement method that the device of micro-momentum is rocked in measurements based on linear frequency modulation multi-beam laser heterodyne described in this embodiment and embodiment four is, signal processing system 10 according to the pivot angle θ ' of the continuous electric signal acquisition Standard Beam 3 receiving by following process implementation:

When the lasting linear frequency modulation laser of launching of linear frequency modulation laser instrument 5 is with incidence angle θ ₀oblique incidence is during to plane standard mirror 7, and the incident field E (t) of plane standard mirror 7 is:

E (t)=E ₀exp{i (ω ₀t+k ' t ²) (formula three),

Wherein, for the rate of change of modulating bandwidth, T is the frequency modulation cycle, and △ F is modulating bandwidth, E ₀for incident field amplitude, t is the time, ω ₀for incident field angular frequency, i represents imaginary number,

If it is l that linear frequency modulation laser arrives the light path of plane standard mirror 7 front surfaces, linear laser of frequency modulation of t-l/c moment arrives the reflection light field E of plane standard mirror 7 front surfaces ₁(t) be:

$E_1\left(t\right)={\mathrm{\α}}_1{E}_0\exp \left\{i\right[{\mathrm{\ω}}_0(t-\frac{l}{c})+k^{\′}{(t-\frac{l}{c})}^2\left]\right\}$ (formula four),

The light of plane standard mirror 7 front surface transmissions is not all being carried out multiple reflections and refraction by the front surface of plane standard mirror 7 and rear surface in the same time, and the catoptrical light field that reflection obtains is each time:

$\left\{\begin{array}{c}{E}_2\left(t\right)={\mathrm{\α}}_2{E}_0\exp \left\{i\right[{\mathrm{\ω}}_0(t-\frac{l+2\mathrm{nd}\cos \mathrm{\θ}}{c})+k^{\′}{(t-2\mathrm{nd}\cos \mathrm{\θ})}^2+\frac{2{\mathrm{\ω}}_0\mathrm{nd}\cos \mathrm{\θ}}{c}\left]\right\}\\ E_3\left(t\right)={\mathrm{\α}}_3{E}_0\exp \left\{i\right[{\mathrm{\ω}}_0(t-\frac{l+4\mathrm{nd}\cos \mathrm{\θ}}{c})+k^{\′}{(t-\frac{l+4\mathrm{nd}\cos \mathrm{\θ}}{c})}^2+\frac{4{\mathrm{\ω}}_0\mathrm{nd}\cos \mathrm{\θ}}{c}\left]\right\}\\ .\\ .\\ .\\ E_m=\left(t\right)={\mathrm{\α}}_m{E}_0\exp \left\{i\right[{\mathrm{\ω}}_0(t-\frac{l+2(m-1)\mathrm{nd}\cos \mathrm{\θ}}{c})+k^{\′}{(t-\frac{l+2(m-1)\mathrm{nd}\cos \mathrm{\θ}}{c})}^2+\frac{2(m-1){\mathrm{\ω}}_0\mathrm{nd}\cos \mathrm{\θ}}{c}\left]\right\}\\ .\\ .\\ .\end{array}\right.$

(formula five),

Wherein, m is nonnegative integer, α ₁=r, α _m=β β ' r ' ^(2m-3)(m>=2), r is the reflectivity of light while injecting plane standard mirror 7 from surrounding medium, β is the transmissivity of light while injecting plane standard mirror 7 from surrounding medium, r ' is the reflectivity of plane standard mirror 7 rear surfaces, transmissivity when β ' is injected into surrounding medium for light from plane standard mirror 7 inside, and d is plane standard mirror 7 thickness, θ is refraction angle, n is plane standard mirror 7 refractive indexes, and c is the light velocity

Total light field E ' that photodetector 9 receives is (t):

E ' (t)=E ₁(t)+E ₂(t)+...+E _m(t)+... (formula six),

The photocurrent I that photodetector 9 is exported is:

$I=\frac{\mathrm{\ηe}}{\mathrm{hv}}\frac{1}{Z}\underset{D}{\∫\∫}\frac{1}{2}[E_1\left(t\right)+E_2\left(t\right)+...+E_m\left(t\right)+...]{[E_1\left(t\right)+E_2\left(t\right)+...+E_m\left(t\right)+...]}^{*}\mathrm{ds}$ (formula seven),

Wherein, e is electron charge, and Z is the intrinsic impedance of photodetector 9 surface dielectrics, and η is quantum efficiency, and D is the area of photodetector 9 photosurfaces, and h is Planck's constant, and v is laser frequency, represents complex conjugate No. *,

Obtain electric current of intermediate frequency I according to formula seven _iFfor:

$I_{\mathrm{IF}}=\frac{\mathrm{\ηe}}{2\mathrm{hv}}\frac{1}{Z}\underset{D}{\∫\∫}\underset{p=0}{\overset{m-1}{\mathrm{\Σ}}}\underset{j=0}{\overset{m-p}{\mathrm{\Σ}}}(E_j\left(t\right){E_{j+p}}^{*}\left(t\right)+{E_j}^{*}\left(t\right)E_{j+p}\left(t\right))\mathrm{ds}$ (formula eight),

By in formula four and formula five substitution formula eight, arrange:

$I_{\mathrm{IF}}=\frac{\mathrm{\ηe}}{\mathrm{hv}}\frac{\mathrm{\π}}{Z}{E}_0^2\underset{p=0}{\overset{m-1}{\mathrm{\Σ}}}\underset{j=0}{\overset{m-p}{\mathrm{\Σ}}}{\mathrm{\α}}_{j+p}{\mathrm{\α}}_j\cos (\frac{4p{k}^{\′}\mathrm{nd}\cos \mathrm{\θ}}{c}t-\frac{4p{k}^{\′}\mathrm{nd}\cos \mathrm{\θ}(l+\mathrm{nd}\cos \mathrm{\θ})}{c^2})$ (formula nine),

Intermediate frequency item difference on the frequency in formula nine is carried out to Fourier transform, obtain the frequency f of interference signal _pfor:

$f_p=\frac{2{\mathrm{pk}}^{\′}\mathrm{nd}\cos \mathrm{\θ}}{\mathrm{\πc}}=K_p\cos \mathrm{\θ}$ (formula ten),

Thereby obtain the value of refraction angle θ, wherein K _pfor scale-up factor, and

According to the known refraction angle θ of refraction law and incidence angle θ ₀pass be:

θ ₀=arcsin (nsin θ) (formula 11),

According to the known incidence angle θ of input path geometric relationship ₀with the pass of the pivot angle θ ' of Standard Beam 3 be:

${\mathrm{\θ}}^{\′}=\frac{{\mathrm{\θ}}_0}{2}=\frac{\arcsin \left(n\sin \mathrm{\θ}\right)}{2}$ (formula 12),

By in the value substitution formula two of the pivot angle θ ' of the Standard Beam 3 obtaining in formula 12, micro-momentum I ' that the laser that acquisition pulsed laser 1 sends and 2 effects of working medium target produce.

In present embodiment, add the variation of Standard Beam 3 front and back system cycles by measurement, calibrate the moment of inertia of system, can obtain Proportional coefficient K according to calibration result _pvalue.

The device of micro-momentum is rocked in linear frequency modulation multi-beam laser heterodyne measurement shown in Fig. 1, under the condition of work of 10Pa, utilize MATLAB analogue measurement working medium for PVC (Polyvinylchloride)+2%C, thickness is 180 μ m, laser initial current is 5A, pulsewidth is 50ms, micro-momentum that laser and working medium interaction produce, and verify the possibility of linear frequency modulation multi-beam laser heterodyne measuring method; get Standard Beam 3 length D=15cm; refractive index n=1.493983 of plane standard mirror, thickness is 3cm; Linear frequency modulation laser wavelength is 1.55 μ m, scan period T=1ms, modulation band-width △ F=5GHz.

Emulation has obtained different incidence angles θ ₀in situation, linear frequency modulation multi-beam laser heterodyne is measured Fourier transform frequency spectrum corresponding to minute angle as shown in Figure 3, as can be seen from Figure 3, and along with incidence angle θ ₀increase, the relative position of frequency spectrum moves to low frequency direction, along with incidence angle θ ₀increase, frequency reduces.This be because, at Proportional coefficient K _pin constant situation, due to the frequency f of interference signal _pwith incidence angle θ ₀pass be f _p=K _pcos θ=K _pcos[arcsin (sin θ ₀/ n)], incidence angle θ ₀frequency f with interference signal _pthe relation that is inversely proportional to, works as incidence angle θ ₀when increase, cos θ reduces thereupon, therefore, and along with incidence angle θ ₀increase, the relative position of frequency spectrum moves to low frequency direction.

Utilize measuring method of the present invention, eight groups of data of continuous coverage, have obtained different incidence angles θ ₀the simulated measurement result of the micro-momentum of testing sample in situation, as shown in the table:

The emulation experiment data of table in utilization, calculate the average measurement value of micro-momentum, the maximum relative error of the measured value finally obtaining is less than 0.48%, simultaneously, the in the situation that of small angle approximation, the systematic error that environment brings and reading error are negligible in emulation, the trueness error after the error in emulation experiment mainly changes from fast Fourier and the round-off error in computation process.

Claims (5)

1. the device of micro-momentum is rocked in the measurement of linear frequency modulation multi-beam laser heterodyne, it is characterized in that, it comprises linear frequency modulation laser instrument (5), the first plane mirror (6), the second plane mirror (4), plane standard mirror (7), Standard Beam (3), vacuum chamber (11), pulsed laser (1), working medium target (2), convergent lens (8), photodetector (9) and signal processing system (10)

Described linear frequency modulation laser instrument (5), the first plane mirror (6), the second plane mirror (4), plane standard mirror (7), Standard Beam (3), pulsed laser (1), working medium target (2) and convergent lens (8) are all placed in vacuum chamber (11)

The center of described Standard Beam (3) is fixed with turning axle,

Described working medium target (2) is pasted the upper surface in Standard Beam (3), the second plane mirror (4) is pasted the lower surface in Standard Beam (3), and working medium target (2) and the second plane mirror (4) are all positioned at same one end of Standard Beam (3)

The laser action that pulse laser is launched produces plasma spraying in working medium target (2), the effect of regurgitating rotates Standard Beam (3), when Standard Beam (3) rotates, linear frequency modulation laser instrument (5) continues to launch linear frequency modulation laser, linear frequency modulation laser is incident to plane standard mirror (7) after the first plane mirror (6) and the second plane mirror (4) reflection, the front surface of plane standard mirror (7) and rear surface are all reflected linear frequency modulation laser and are passed through convergent lens (8) and converge on the photosurface of photodetector (9), the electrical signal of photodetector (9) is connected with the electric signal input end of signal processing system (10).

2. the device of micro-momentum is rocked in linear frequency modulation multi-beam laser heterodyne according to claim 1 measurement, it is characterized in that, described signal processing system (10) comprises wave filter (10-1), prime amplifier (10-2), A/D converter (10-3) and DSP (10-4), the electric signal input end of wave filter (10-1) is connected with the electrical signal of photodetector (9) as the electric signal input end of signal processing system (10), the filtering signal output terminal of wave filter (10-1) is connected with the filtering signal input end of prime amplifier (10-2), the amplifying signal output terminal of prime amplifier (10-2) is connected with the input end of analog signal of A/D converter (10-3), the digital signal output end of A/D converter (10-3) is connected with the digital signal input end of DSP (10-4).

3. the device of micro-momentum is rocked in linear frequency modulation multi-beam laser heterodyne according to claim 1 measurement, it is characterized in that, described vacuum chamber has vacuum window on (11), and described vacuum window is used for making the light in vacuum chamber (11) to assemble photodetector (9) photosurface outside to vacuum chamber (11).

Linear frequency modulation multi-beam laser heterodyne measurement based on described in claim 1 or 2 rock micro-momentum device rock micro-impulse measurement method, it is characterized in that, it is by following process implementation:

Pulsed laser (1), linear frequency modulation laser instrument (5), photodetector (9) and signal processing system (10) are switched to duty, photodetector (9) is converted to electric signal by the light signal receiving and is sent to signal processing system (10), signal processing system (10) obtains the pivot angle θ ' of Standard Beam (3) according to the continuous electric signal receiving

According to:

$I^{\′}=\frac{2\mathrm{J\ω}}{D}\·{\mathrm{\θ}}^{\′}=\frac{4\mathrm{\πJ}}{{\mathrm{DT}}^{\′}}\·{\mathrm{\θ}}^{\′}$ (formula one),

Micro-momentum I ' that the laser that acquisition pulsed laser (1) sends and working medium target (2) effect produce, wherein, J is the moment of inertia of the system of rocking, ω is damped frequency, and T ' is damping period, and D is Standard Beam (3) length, make k=4 π J/DT ':

I '=ki θ ' (formula two).

According to claim 4 based on linear frequency modulation multi-beam laser heterodyne measurement rock micro-momentum device rock micro-impulse measurement method, it is characterized in that, signal processing system (10) obtains Standard Beam (3) pivot angle θ ' according to the continuous electric signal receiving is by following process implementation:

When the lasting linear frequency modulation laser of launching of linear frequency modulation laser instrument (5) is with incidence angle θ ₀oblique incidence is during to plane standard mirror (7), and the incident field E (t) of plane standard mirror (7) is:

E (t)=E ₀exp{i (ω ₀t+k ' t ²) (formula three),

Wherein, for the rate of change of modulating bandwidth, T is the frequency modulation cycle, and △ F is modulating bandwidth, E ₀for incident field amplitude, t is the time, ω ₀for incident field angular frequency, i represents imaginary number,

If it is l that linear frequency modulation laser arrives the light path of plane standard mirror (7) front surface, linear laser of frequency modulation of t-l/c moment arrives the reflection light field E of plane standard mirror (7) front surface ₁(t) be:

$E_1\left(t\right)={\mathrm{\α}}_1{E}_0\exp \left\{i\right[{\mathrm{\ω}}_0(t-\frac{l}{c})+k^{\′}{(t-\frac{l}{c})}^2\left]\right\}$ (formula four),

The light of plane standard mirror (7) front surface transmission is not all being carried out multiple reflections and refraction by the front surface of plane standard mirror (7) and rear surface in the same time, and the catoptrical light field that reflection obtains is each time:

$\left\{\begin{array}{c}{E}_2\left(t\right)={\mathrm{\α}}_2{E}_0\exp \left\{i\right[{\mathrm{\ω}}_0(t-\frac{l+2\mathrm{nd}\cos \mathrm{\θ}}{c})+k^{\′}{(t-2\mathrm{nd}\cos \mathrm{\θ})}^2+\frac{2{\mathrm{\ω}}_0\mathrm{nd}\cos \mathrm{\θ}}{c}\left]\right\}\\ E_3\left(t\right)={\mathrm{\α}}_3{E}_0\exp \left\{i\right[{\mathrm{\ω}}_0(t-\frac{l+4\mathrm{nd}\cos \mathrm{\θ}}{c})+k^{\′}{(t-\frac{l+4\mathrm{nd}\cos \mathrm{\θ}}{c})}^2+\frac{4{\mathrm{\ω}}_0\mathrm{nd}\cos \mathrm{\θ}}{c}\left]\right\}\\ .\\ .\\ .\\ E_m=\left(t\right)={\mathrm{\α}}_m{E}_0\exp \left\{i\right[{\mathrm{\ω}}_0(t-\frac{l+2(m-1)\mathrm{nd}\cos \mathrm{\θ}}{c})+k^{\′}{(t-\frac{l+2(m-1)\mathrm{nd}\cos \mathrm{\θ}}{c})}^2+\frac{2(m-1){\mathrm{\ω}}_0\mathrm{nd}\cos \mathrm{\θ}}{c}\left]\right\}\\ .\\ .\\ .\end{array}\right.$

(formula five),

Wherein, m is nonnegative integer, α ₁=r, α _m=β β ' r ' ^(2m-3)(m>=2), r is the reflectivity of light while injecting plane standard mirror (7) from surrounding medium, β is the transmissivity of light while injecting plane standard mirror (7) from surrounding medium, r ' is the reflectivity of plane standard mirror (7) rear surface, transmissivity when β ' is injected into surrounding medium for light from plane standard mirror (7) inside, d is plane standard mirror (7) thickness, θ is refraction angle, n is plane standard mirror (7) refractive index, c is the light velocity

Total light field E ' that photodetector (9) receives is (t):

E ' (t)=E ₁(t)+E ₂(t)+...+E _m(t)+... (formula six),

The photocurrent I of photodetector (9) output is:

$I=\frac{\mathrm{\ηe}}{\mathrm{hv}}\frac{1}{Z}\underset{D}{\∫\∫}\frac{1}{2}[E_1\left(t\right)+E_2\left(t\right)+...+E_m\left(t\right)+...]{[E_1\left(t\right)+E_2\left(t\right)+...+E_m\left(t\right)+...]}^{*}\mathrm{ds}$ (formula seven),

Wherein, e is electron charge, and Z is the intrinsic impedance of photodetector (9) surface dielectric, and η is quantum efficiency, and D is the area of photodetector (9) photosurface, and h is Planck's constant, and v is laser frequency, represents complex conjugate No. *,

Obtain electric current of intermediate frequency I according to formula seven _iFfor:

$I_{\mathrm{IF}}=\frac{\mathrm{\ηe}}{2\mathrm{hv}}\frac{1}{Z}\underset{D}{\∫\∫}\underset{p=0}{\overset{m-1}{\mathrm{\Σ}}}\underset{j=0}{\overset{m-p}{\mathrm{\Σ}}}(E_j\left(t\right){E_{j+p}}^{*}\left(t\right)+{E_j}^{*}\left(t\right)E_{j+p}\left(t\right))\mathrm{ds}$ (formula eight),

By in formula four and formula five substitution formula eight, arrange:

$I_{\mathrm{IF}}=\frac{\mathrm{\ηe}}{\mathrm{hv}}\frac{\mathrm{\π}}{Z}{E}_0^2\underset{p=0}{\overset{m-1}{\mathrm{\Σ}}}\underset{j=0}{\overset{m-p}{\mathrm{\Σ}}}{\mathrm{\α}}_{j+p}{\mathrm{\α}}_j\cos (\frac{4p{k}^{\′}\mathrm{nd}\cos \mathrm{\θ}}{c}t-\frac{4p{k}^{\′}\mathrm{nd}\cos \mathrm{\θ}(l+\mathrm{nd}\cos \mathrm{\θ})}{c^2})$ (formula nine),

Intermediate frequency item difference on the frequency in formula nine is carried out to Fourier transform, obtain the frequency f of interference signal _pfor:

$f_p=\frac{2{\mathrm{pk}}^{\′}\mathrm{nd}\cos \mathrm{\θ}}{\mathrm{\πc}}=K_p\cos \mathrm{\θ}$ (formula ten),

Thereby obtain the value of refraction angle θ, wherein K _pfor scale-up factor, and

According to the known refraction angle θ of refraction law and incidence angle θ ₀pass be:

θ ₀=arcsin (nsin θ) (formula 11),

According to the known incidence angle θ of input path geometric relationship ₀with the pass of the pivot angle θ ' of Standard Beam (3) be:

${\mathrm{\θ}}^{\′}=\frac{{\mathrm{\θ}}_0}{2}=\frac{\arcsin \left(n\sin \mathrm{\θ}\right)}{2}$ (formula 12),

By in the value substitution formula two of the pivot angle θ ' of the Standard Beam (3) obtaining in formula 12, micro-momentum I ' that the laser that acquisition pulsed laser (1) sends and working medium target (2) effect produce.