General influence of atmosphere refraction
- Two velocity in atmosphere: phase and group velocity
- Background: a simple harmonic wave propagating in air looks like u(x,t)=A0∗sin(ωt−kx+ϕ0)u(x,t)=A0∗sin(ωt−kx+ϕ0), where ωω is angular frequency, represented in radians per second, k is angular wavenumber, represented in radians per meter.
- group velocity is the propagating speed of an evenlope wave, which is modulated(overlap several waves) to carry information. On the contrary, a simple harmonic wave(showed before) can not carry any information.
- Phase velocity: vph=ω/k=λ/Tvph=ω/k=λ/T
- Relationship between group velocity and phase velocity:vgr=vph−ω∗dvphdωvgr=vph−ω∗dvphdω
- This means when vphvph is independent with the wavelength(no dispersion), then vgr=vphvgr=vph.
- Structure of atmosphere: troposphere and ionosphere
- troposphere: ranging from 0km to 10 km above the ground
- Note that for microwave the tropospheric refraction is non-dispersive. This means the signal delay caused in troposphere in this frequency range is irrelevant with the frequency.
- While for optical range the tropospheric refraction is frequency-dependent and non-dispersive.
- ionosphere: range from 50km to 1000km above the ground
- the free electrons and ions in ionosphere is related to the solar radiation.
- troposphere: ranging from 0km to 10 km above the ground
- The signal delay δρatm=∫L(n(s)−1)ds+(S−G)δρatm=∫L(n(s)−1)ds+(S−G)
- Here, S is the curved path of propagating light, while G is the geometric distance.
- The first term can achieved highly at 200m, while the latter is negilible (excepet for low zenith angle) , 1 to 2 centimeter.
- Generally speaking the refractive index depends on frequency. By definition nph=c/vphnph=c/vph and ngr=c/vgrngr=c/vgr.
Ionospheric refraction correction
- Ionospheric Refraction: phase advance, group delay
- For frequency bigger than 100MHz, the mathematical model of Ionospheric refraction: nph=1−a∗Nef2nph=1−a∗Nef2 and ngr=1+a∗Nef2ngr=1+a∗Nef2 Dispersive!!: depends on the frequency
- a is constant: a=a=40.3m3s−2a=a=40.3m3s−2; NeNe refers to the free electrons density along signal path.
- Correction for ionospheric refraction: δρph=−a∗Ef2δρph=−a∗Ef2
δρgr=a∗Ef2δρgr=a∗Ef2
Here E denotes the Total Electron Content: E=∫Ne(s)dsE=∫Ne(s)ds - ionospheric refraction correction is negative for phase measurement (phase advance), while positive for code/pseudorange measurement(group delay).
- Mostly only the VTEC (Vertical Total Electrons Content) EVEV is provided, to get E in a specific direction we need a map function.(See page 101)
- Final formula:δρph=−a∗mion(z)EVf2=−a∗1cosz∗EVf2δρph=−a∗mion(z)EVf2=−a∗1cosz∗EVf2
- Using the above formula, we assume all electron concentrated in an infinitesimally thin layer above the earth surface.
- The smaller the frequency, the bigger the inonspheric correction. So for GNSS (L-Band) is 1 - 15m. For VLBI using X-Band is much smaller: 4cm - 60cm. For Altimetry (X or Ku-Band) is 1 cm - 15 cm.
- For SLR/LLR which employ optical wave (frequency: 5∗10145∗1014) the delay casued by ionospheric refraction is negilible.
- Ionospheric-free linear combination to eliminate the ionospheric delay.
Tropospheric delay for radio wave: Dry part or Wet part
- For radio waves range from 100MHz to 15GHz the tropospheric delay is non-disperive. While for optical signal is dispersive.
- Tropospheric delay can still be modelled as δρtro=∫(n(s)−1)dsδρtro=∫(n(s)−1)ds. Here we introduce refractivity N=106∗(n−1)N=106∗(n−1). So δρtro=10−6∫N(s)dsδρtro=10−6∫N(s)ds
- Model of refractivity: N=Nd+Nw=k1∗PdT∗Z(−1)d+k2∗eT∗Z(−1)w+k3∗eT2∗Z(−1)wN=Nd+Nw=k1∗PdT∗Zd(−1)+k2∗eT∗Zw(−1)+k3∗eT2∗Zw(−1)
- Refractivity not only depends on pressure and compressibility of air, but also depends on electrical characterstics of molecules, where N2N2 or O2O2 are different with H2OH2O.
- e : partial pressure of water vapour, a function of relative humidity
- Total delay amounts to 2.3m in zenith direction, and about 25 at an elevation of 5 degree.
- Dry part contributes to 90% of tropospheric delay, and can be modelled quite well based on the pressure measurment on the ground, and changes rather slowly.
- Wet part amounts to maximum about 40 cm, but is highly variable in time and space.
- Tropospheric delay can be writen as the product of zenith delay and map function mtrp(z)mtrp(z). Normally the mapping function for dry part and wet part is different. So the following formular is given: δρtro=mtrp,d(z)∗δρ0tro,d+mtrp,w(z)∗δρ0tro,wδρtro=mtrp,d(z)∗δρtro,d0+mtrp,w(z)∗δρtro,w0
- Tropospheric correction can be modelled based on meterological data including air pressure P, temperature T and relative humidity H(Using water vapor radiometry). You can also based on standard meterologival model, but is not accurate enough.
Tropospheric delay for optical part of spectrum (SLR/LLR)
- As for tropospheric delay for optic wave, the contribution of dry part (partial pressure of dir air) is one order higher than the wet part(partial pressure of water vapour)
- The distance correction at normal condition in zenith direction amounts to 2.45m and 7m at the elevation angle of 20 degree.
- The magnitude of tropospheric correction of dry part for optical and radio wave are similar(2.3 -2.4m). While for wet part, optical is much smaller(up to 5mm).
- a change of meterological condition result in a change of tropospheric correction at several mm level, due to the low coefficient of wet air pressure. Tropospheric correction for optical wave is less variable.
- Thus troposhperic delay can be modelled sufficiently accurately based on the meterological measurement at station.
- By contrast, for VLBI or GPS, the change of meterological condition result in significant change of tropospheric correction(up to 40cm).
Estimation of troposphere Parameter: zenith troposphere delay
- Normally ZTD is estimated for every station involved and is valid for 30mins to 120mins.
- By contrast, for the influence of dry part of tro towards radio waves the pressure measurment is valid 12hours, with a resulting error less than 2cm.
- The main problem of tro parameter estimation is the correlation between the parameters, because they all change with the change of zenith angle
- station height
- receiver clock correction
- troposphere delay
- phase ambiguities
- offset and variation of antenna phase centers
- Ways to eliminate correlation:
- at least 1-2 hours observation
- in static mode
- open sky(good satellite geometry)
- Typically estimate one ZTD per hour