CN103838968A - Low-elevation-angle tropospheric refraction correction method - Google Patents

Low-elevation-angle tropospheric refraction correction method Download PDF

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CN103838968A
CN103838968A CN201410069905.4A CN201410069905A CN103838968A CN 103838968 A CN103838968 A CN 103838968A CN 201410069905 A CN201410069905 A CN 201410069905A CN 103838968 A CN103838968 A CN 103838968A
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iteration
angle
tropospheric
signal
earth
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周率
曹建峰
韩松涛
程国胜
孙靖
师明
刘荟萃
李黎
辛望
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Beijing Aerospace Control Center
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Abstract

The invention belongs to the technical field of atmospheric sciences and discloses a low-elevation-angle tropospheric refraction correction method. The low-elevation-angle tropospheric refraction correction method comprises the steps of 1 calculating a ray trajectory of a tropospheric propagated low-elevation-angle measurement signal; 2 establishing a low-elevation-angle tropospheric refraction correction iteration algorithm; 3 confirming a low-elevation-angle tropospheric refraction correction iteration stopping condition; 4 calculating the low-elevation-angle tropospheric refraction correction amount. By adopting the low-elevation-angle tropospheric refraction correction method, the refraction correction accuracy of the low-elevation-angle measurement signal passing through a troposphere is improved, the effects of spaceflight test control, navigational positioning and the like are effectively improved, and technical support is provided for the fields of spaceflight test control, communication and navigation and the like in our country.

Description

A kind of low elevation angle tropospheric refraction modification method
Technical field
The invention belongs to atmospheric science technical field, relate to a kind of low elevation angle tropospheric refraction modification method.
Background technology
The aircraft such as spacecraft, guided missile all will experience atmosphere convection layer, the refraction effect of atmosphere cause delay that electricity (light) ripple is propagated and path bending and cause error, be to improve the effective means of telemetry communication, navigation and positioning accuracy to the error correction of signal communication media.In the practical engineering application such as space flight measurement and control, tropospheric refraction corrected Calculation adopts the refraction model based on atmosphere spherically stratified ionosphere hypothesis, suppose that the earth is ball, atmospheric strument is uniform in the horizontal direction, atmospheric refraction on position angle without impact, only consider range finding and the error correction of the angle of pitch, atmosphere can be divided into concentric thin layer along sphere, and the integration modification methods such as hopfield based on spherically stratified ionosphere are conventional convection current modification methods.
Under this hypothesis of atmosphere sphere Hierachical Basis, the earth is ball, and its mean radius is t e, the thin layer radius concentric with the earth is r.In troposphere, the calculation of parameter such as thin layer radius (the earth's core distance) the atmospheric temperature in r place, humidity and the air pressure that signal refractive index n (r) is concentric according to the earth obtain, and without loss of generality, in engineering, refractive index n are abbreviated as to the function of r:
n=n(r) (9)
And electric wave and light wave meet Snell law at the propagation law in space, in the concentric atmosphere thin layer of any one and the earth, set up:
nrcosθ=const (10)
Wherein, n is the refractive index in thin layer, and r is thin layer radius, and θ is the angle of signal ray and thin layer tangent plane, as shown in Figure 1.In Fig. 1
Figure BSA0000101474390000024
for the earth's core angle, S is geometric distance.
Traditional troposphere integration correction algorithm is generally taking the earth's core on swash travel path apart from as integration variable, its earth's core angle
Figure BSA0000101474390000025
computing formula be:
Figure BSA0000101474390000021
Wherein, r 0for the earth's core distance at survey station place, n 0for the refractive index at survey station place, E is the apparent elevation angle at survey station place; r mfor the earth's core distance at target place, n is that the earth's core is apart from the refractive index at r place.When E hour, denominator is tending towards 0 and can makes integral result error very large.Therefore in engineering application, the tropospheric refraction correction of the lower measuring-signal in the low elevation angle (≤10 °) is a technical barrier, and the low elevation angle is that the measurement and control signal direction of survey station transmitting and the angle of horizontal direction are not more than 10 °.
Summary of the invention
The problem that the present invention need to solve is: provide a kind of low elevation angle tropospheric refraction modification method, to improve the correction precision of signal at tropospheric propagation.
For solving the problems of the technologies described above, the present invention proposes a kind of low elevation angle tropospheric refraction modification method, comprises the following steps:
Step 1, set up the ray tracing system of equations of low measurement of elevation signal at tropospheric propagation
Low measurement of elevation signal is as follows in the ray tracing system of equations of tropospheric propagation:
Figure DEST_PATH_GSB0000124542000000015
Wherein, to be low measurement of elevation signal propagate the angle of atmospheric envelope tangent plane at the ray of tropospheric propagation and signal to θ, and r is that signal is propagated atmospheric radius, the infinitesimal that ds gets on the ray geometric distance S of tropospheric propagation for signal,
Figure BSA0000101474390000034
for the earth's core angle between survey station and target, n (r) refractive index that to be signal propagate at atmospheric envelope, R is and the actual propagation path of ds respective signal.
Step 2, set up low elevation angle tropospheric refraction correction iterative algorithm
The thought of iteration correction is to choose suitable step-length, make to revise precision reach demand by iterating, and the low elevation angle tropospheric refraction correction iterative algorithm of foundation is as follows:
2.1, k=0, getting iteration step length is Δ S, obtains iterative initial value system of equations as follows:
Figure BSA0000101474390000031
Wherein, r 0for the earth's core distance of survey station, r afor the earth's core distance of target,
Figure BSA0000101474390000032
for the earth's core angle of real survey station and target, R 0for real range finding, θ 0for signal is propagated atmospheric envelope tangent plane angle, E at real ray and the signal of tropospheric propagation efor survey station place is without the actual measurement elevation angle of refraction correction.
2.2, k=k+1, obtains the iterative algorithm system of equations of revising in troposphere as follows:
Figure BSA0000101474390000033
Wherein, r k, r k-1be respectively the earth's core distance of iteration k step and k-1 step target, Δ S is iteration step length, θ k, θ k-1respectively that iteration k step and k-1 step signal are propagated atmospheric envelope tangent plane angle at ray and the signal of tropospheric propagation,
Figure BSA0000101474390000041
respectively iteration k step and the survey station of k-1 step and the earth's core angle of target, R k, R k-1respectively the range finding of iteration k step and k-1 step, n (r k), n (r k-1) be respectively the signal refractive index of iteration k step and k-1 step.
Step 3, determine low elevation angle tropospheric refraction correction stopping criterion for iteration
The checking system of equations that stops low elevation angle tropospheric refraction correction iteration is as follows:
R k ≤ R e R k + n ( r k ) ΔS > R e
Wherein, R kthe range finding of iteration k step, R efor the range finding that survey station place is revised without refraction, n (r k) be the signal refractive index of iteration k step, Δ S is iteration step length.
Step 4, calculate low elevation angle tropospheric refraction correction
Calculate low elevation angle tropospheric refraction correction as follows:
ΔE = E e - E 0 ΔR = R e - R 0
Wherein Δ E is elevation angle correction, and Δ R is range finding correction, R ewith E ebe respectively measured distance and the actual measurement elevation angle revised without refraction at survey station place, R 0with E 0be respectively real range finding and the elevation angle.
Figure BSA0000101474390000044
Wherein, r afor the earth's core distance of iteration target when initial.R end,
Figure BSA0000101474390000045
and θ endbe respectively the earth's core angle of low elevation angle tropospheric refraction correction iteration target the earth's core while finishing apart from, survey station and target, and the apparent elevation angle at target place, its computing formula is as follows:
Figure BSA0000101474390000051
Wherein, r kfor target the earth's core distance of iteration k step, θ kfor the apparent elevation angle at iteration k step target place, for the earth's core angle of iteration k pacing station and target, R kfor the range finding of iteration k step, n (r k) be the refractive index of iteration k step.Δ S lastfor the step-length of last iteration, its computing formula is as follows:
△S last=R e-R k
Wherein, R e, R kbe respectively survey station place without the range finding of refraction correction and the range finding of iteration k step.
The technology of the present invention beneficial effect:
The present invention is on based on atmosphere sphere theory of hierarchies basis, set up the ray tracing system of equations of signal at tropospheric propagation, and research iterative algorithm, set up low elevation angle tropospheric refraction correction iterative algorithm, not only calculate low elevation angle tropospheric refraction modified value, calculated range finding modified value simultaneously, and by theory and experimental verification, adopt the inventive method to realize the low elevation angle of raising signal tropospheric propagation correction precision, for the fields such as China's space flight measurement and control, communication and navigation provide technical support.
Brief description of the drawings
Fig. 1 is that signal is propagated schematic diagram at earth concentric circles thin layer.
Fig. 2 is the low elevation angle of the present invention tropospheric refraction modification method process flow diagram.
Fig. 3 is low measurement of elevation signal tropospheric refraction correction effect figure in the embodiment of the present invention.
Embodiment
Below in conjunction with accompanying drawing, the present invention is described further.
As shown in Figure 2, the low elevation angle of one of the present invention tropospheric refraction modification method, comprises the steps:
Step 1, set up the ray tracing system of equations of low measurement of elevation signal at tropospheric propagation
Low measurement of elevation signal is as follows in the ray tracing system of equations of tropospheric propagation:
Figure DEST_PATH_GSB0000124542000000021
Wherein, to be low measurement of elevation signal propagate the angle of atmospheric envelope tangent plane at the ray of tropospheric propagation and signal to θ, and r is that signal is propagated atmospheric radius, the infinitesimal that ds gets on the ray geometric distance S of tropospheric propagation for signal,
Figure BSA0000101474390000063
for the earth's core angle between survey station and target, n (r) refractive index that to be signal propagate at atmospheric envelope, R is and the actual propagation path of ds respective signal.
In system of equations (1), (1-1) formula, (1-2) formula, (1-3) formula are the signal that obtained by the formula of mentioning in background technology (9) and Fig. 1 ray geometric relationships at tropospheric propagation.
(1-4) formula is by after the differential of formula (10) both sides, then is simplified and obtained by geometric relationship, specific as follows:
To formula (10) both sides simultaneously to ds differential, n=n (r):
Figure BSA0000101474390000062
By (1-1) formula substitution (2) formula, simplify (1-4) formula that obtains.System of equations (1) can be described under the low elevation angle the uniform measuring-signal of horizontal refraction in the ray tracing of tropospheric propagation.
Step 2, set up low elevation angle tropospheric refraction correction iterative algorithm
The thought of iteration correction is to choose suitable step-length, make to revise precision reach demand by iterating, and the low elevation angle tropospheric refraction correction iterative algorithm of foundation is as follows:
2.1, k=0, getting iteration step length is Δ S, obtains iterative initial value system of equations as follows:
Figure BSA0000101474390000071
Wherein, r 0for the earth's core distance of survey station, r afor the earth's core distance of target,
Figure BSA0000101474390000074
for the earth's core angle of real survey station and target, R 0for real range finding, θ 0for signal is propagated atmospheric envelope tangent plane angle, E at real ray and the signal of tropospheric propagation efor survey station place is without the actual measurement elevation angle of refraction correction.
2.2, k=k+1, obtains the iterative algorithm system of equations of revising in troposphere as follows:
Figure BSA0000101474390000072
Wherein, r k, r k-1be respectively the earth's core distance of iteration k step and k-1 step target, Δ S is iteration step length, θ k, θ k-1respectively that iteration k step and k-1 step signal are propagated atmospheric envelope tangent plane angle at ray and the signal of tropospheric propagation,
Figure BSA0000101474390000073
respectively iteration k step and the survey station of k-1 step and the earth's core angle of target, R k, R k-1respectively the range finding of iteration k step and k-1 step, n (r k), n (r k-1) be respectively the signal refractive index of iteration k step and k-1 step.
Step 3, determine low elevation angle tropospheric refraction correction stopping criterion for iteration
The checking system of equations that stops low elevation angle tropospheric refraction correction iteration is as follows:
R k ≤ R e R k + n ( r k ) ΔS > R e - - - ( 5 )
Wherein, R kthe range finding of iteration k step, R efor the range finding that survey station place is revised without refraction, n (r k) be the signal refractive index of iteration k step, Δ S is iteration step length.
Step 4, calculate low elevation angle tropospheric refraction correction
Calculate low elevation angle tropospheric refraction correction as follows:
ΔE = E e - E 0 ΔR = R e - R 0 - - - ( 6 )
Wherein Δ E is elevation angle correction, and Δ R is range finding correction, R ewith E ebe respectively measured distance and the actual measurement elevation angle revised without refraction at survey station place, R 0with E 0be respectively real range finding and the elevation angle.
Figure BSA0000101474390000083
Wherein, r afor the earth's core distance of iteration target when initial.R end,
Figure BSA0000101474390000084
and θ endbe respectively the earth's core angle of low elevation angle tropospheric refraction correction iteration target the earth's core while finishing apart from, survey station and target, and the apparent elevation angle at target place, its computing formula is as follows:
Figure BSA0000101474390000085
Wherein, r kfor target the earth's core distance of iteration k step, θ kfor the apparent elevation angle at iteration k step target place,
Figure BSA0000101474390000091
for the earth's core angle of iteration k pacing station and target, R kfor the range finding of iteration k step, n (r k) be the refractive index of iteration k step.Δ S tastfor the step-length of last iteration, its computing formula is as follows:
△S tast=R e-R k
Wherein, R e, R kbe respectively survey station place without the range finding of refraction correction and the range finding of iteration k step.
Choose the aloft low elevation angle observing and controlling period of low flyer No. one time, carry out tropospheric refraction correction by above-mentioned steps of the present invention.It is 2 °~8 ° that the optical device of flight period is measured the elevation angle, and finding range is 10km~30km, the about 1.6km of object height.Fig. 3 is the correction effect figure of signal tropospheric refraction.
As shown in Figure 3, the residual error of iterative algorithm and the residual error of measured data are coincide more satisfactory, it is revised residual error and is significantly less than the conventional hopfield model of engineering, shows that iterative algorithm has higher precision for the tropospheric refraction correction of the low elevation angle, possesses engineering practical value.

Claims (1)

1. a low elevation angle tropospheric refraction modification method, is characterized in that: comprise the steps:
Step 1, to set up low measurement of elevation signal as follows in the ray tracing system of equations of tropospheric propagation at the low measurement of elevation signal of ray tracing system of equations of tropospheric propagation:
Figure DEST_PATH_FSB0000124541990000011
Wherein, to be low measurement of elevation signal propagate the angle of atmospheric envelope tangent plane at the ray of tropospheric propagation and signal to θ, and r is that signal is propagated atmospheric radius, the infinitesimal that ds gets on the ray geometric distance S of tropospheric propagation for signal,
Figure FSA0000101474380000014
for the earth's core angle between survey station and target, n (r) refractive index that to be signal propagate at atmospheric envelope, R is and the actual propagation path of ds respective signal;
Step 2, set up low elevation angle tropospheric refraction correction iterative algorithm
2.1, k=0, getting iteration step length is Δ S, obtains iterative initial value system of equations as follows:
Figure FSA0000101474380000012
Wherein, r 0for the earth's core distance of survey station, r afor the earth's core distance of target,
Figure FSA0000101474380000013
for the earth's core angle of real survey station and target, R 0for real range finding, θ 0for signal is propagated atmospheric envelope tangent plane angle, E at real ray and the signal of tropospheric propagation efor survey station place is without the actual measurement elevation angle of refraction correction;
2.2, k=k+1, obtains the iterative algorithm system of equations of revising in troposphere as follows:
Figure FSA0000101474380000021
Wherein, r k, r k-1be respectively the earth's core distance of iteration k step and k-1 step target, Δ S is iteration step length, θ k, θ k-1respectively that iteration k step and k-1 step signal are propagated atmospheric envelope tangent plane angle at ray and the signal of tropospheric propagation,
Figure FSA0000101474380000024
respectively iteration k step and the survey station of k-1 step and the earth's core angle of target, R k, R k-1respectively the range finding of iteration k step and k-1 step, n (r k), n (r k-1) be respectively the signal refractive index of iteration k step and k-1 step;
Step 3, determine low elevation angle tropospheric refraction correction stopping criterion for iteration
The checking system of equations that stops low elevation angle tropospheric refraction correction iteration is as follows:
Figure FSA0000101474380000022
Wherein, R kthe range finding of iteration k step, R efor the range finding that survey station place is revised without refraction, n (r k) be the signal refractive index of iteration k step, Δ S is iteration step length;
Step 4, calculate low elevation angle tropospheric refraction correction
Calculate low elevation angle tropospheric refraction correction as follows:
Figure FSA0000101474380000023
Wherein, Δ E is elevation angle correction, and Δ R is range finding correction, R ewith E ebe respectively measured distance and the actual measurement elevation angle revised without refraction at survey station place, R 0with E 0be respectively real range finding and the elevation angle:
Figure FSA0000101474380000031
Wherein, r afor the earth's core distance of iteration target when initial.R end,
Figure FSA0000101474380000032
and θ endbe respectively the earth's core angle of low elevation angle tropospheric refraction correction iteration target the earth's core while finishing apart from, survey station and target, and the apparent elevation angle at target place, its computing formula is as follows:
Figure FSA0000101474380000033
Wherein, r kfor target the earth's core distance of iteration k step, θ kfor the apparent elevation angle at iteration k step target place,
Figure FSA0000101474380000034
for the earth's core angle of iteration k pacing station and target, R kfor the range finding of iteration k step, n (r k) be the refractive index of iteration k step, Δ S tastfor the step-length of last iteration, its computing formula is as follows:
ΔS last=R e-R k
Wherein, R e, R kbe respectively survey station place without the range finding of refraction correction and the range finding of iteration k step.
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CN106052717A (en) * 2016-07-15 2016-10-26 中国西安卫星测控中心 Method for calibrating radio wave refraction correction effects by virtue of precision trajectory
CN106707256A (en) * 2015-07-27 2017-05-24 中国人民解放军信息工程大学 Tropospheric waveguide inversion method and device based on radar sea clutter
CN107563012A (en) * 2017-08-10 2018-01-09 西安电子科技大学 Atmospheric parameters based on curve matching search table generating method
CN109932711A (en) * 2019-04-09 2019-06-25 中国人民解放军63921部队 A kind of refraction correction method of radar surveying
CN111103573A (en) * 2019-10-19 2020-05-05 中国电波传播研究所(中国电子科技集团公司第二十二研究所) Refraction correction method for measuring TDOA (time difference of arrival) based on satellite external radiation source radar
CN112098953A (en) * 2020-09-21 2020-12-18 中国人民解放军63921部队 Rapid iteration method and device for calculating atmospheric refraction correction
CN113093241A (en) * 2021-03-12 2021-07-09 东南大学 Single-survey-station troposphere slope delay calculation method considering elevation angle

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106707256A (en) * 2015-07-27 2017-05-24 中国人民解放军信息工程大学 Tropospheric waveguide inversion method and device based on radar sea clutter
CN106707256B (en) * 2015-07-27 2019-01-25 中国人民解放军信息工程大学 A kind of tropospheric ducting inversion method and device based on radar sea clutter
CN106052717A (en) * 2016-07-15 2016-10-26 中国西安卫星测控中心 Method for calibrating radio wave refraction correction effects by virtue of precision trajectory
CN106052717B (en) * 2016-07-15 2018-12-11 中国西安卫星测控中心 A kind of radio wave refractive correction effect scaling method using accurate trajectory
CN107563012A (en) * 2017-08-10 2018-01-09 西安电子科技大学 Atmospheric parameters based on curve matching search table generating method
CN109932711A (en) * 2019-04-09 2019-06-25 中国人民解放军63921部队 A kind of refraction correction method of radar surveying
CN109932711B (en) * 2019-04-09 2021-02-02 中国人民解放军63921部队 Atmospheric refraction correction method for radar measurement
CN111103573A (en) * 2019-10-19 2020-05-05 中国电波传播研究所(中国电子科技集团公司第二十二研究所) Refraction correction method for measuring TDOA (time difference of arrival) based on satellite external radiation source radar
CN111103573B (en) * 2019-10-19 2021-09-17 中国电波传播研究所(中国电子科技集团公司第二十二研究所) Refraction correction method for measuring TDOA (time difference of arrival) based on satellite external radiation source radar
CN112098953A (en) * 2020-09-21 2020-12-18 中国人民解放军63921部队 Rapid iteration method and device for calculating atmospheric refraction correction
CN113093241A (en) * 2021-03-12 2021-07-09 东南大学 Single-survey-station troposphere slope delay calculation method considering elevation angle
CN113093241B (en) * 2021-03-12 2024-02-02 东南大学 Single-station troposphere oblique delay calculation method considering altitude angle

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