F.2 Greek Symbols

Symbol		Explanation
$\alpha$		angle, right ascension
	$\alpha$	chopper angle
	$\alpha$	x-axis offset of the peak from the centre of the array
	$\alpha_{c}$	right ascension for raster centre
	$\alpha_{m,n}$	right ascension of raster point (m,n)
	$\alpha_{amp}$	chopper amplitude
	$\alpha_{approx}$	approximation to chopper angle
	$\alpha_{linear}$	first approximation to chopper angle from linear model,
	$\alpha_{sky}$	approximation to chopper angle
$\alpha$		probability that null hypothesis is rejected
$\alpha$(f,a)		correction for inhomogeneous illumination in aperture a by FCS
	$\alpha^{f}$(a)	inhomogeneous FCS illumination for PHT-P
$\beta$		y-axis offset of the peak from the centre of the array
$\beta$		power of the dust emissivity
$\Gamma$(i,f)		FCS illumination matrix
	$\Gamma^{f}$(i)	idem
$\delta$		declination
	$\delta_{c}$	declination of raster centre
	$\delta_{m,n}$	declination of raster point (m,n)
$\delta$		degrees of freedom
$\Delta$		Increment, difference, or uncertainty
	$\Delta$l	physical pixel size in Z-direction
	${\Delta}M$, ${\Delta}N$	raster step size in M and N
	$\Delta$x	physical distance between pixels
	$\Delta \lambda$	width of filter bandpass
	$\Delta\lambda_{pix}$	PHT-S pixel width in wavelength
$\epsilon$		central obscuration factor by the secondary mirror
$\zeta$(S)		signal correction function for losses due to chopper modulation
	$\zeta(s_{scr}, det, t_{dwell})$	idem
	$\zeta(S_{src},det,t_{dwell})$	idem
$\iota$		number of interpolations,
$\theta_{chop}$		maximum chopper deflection while mapping (PHT32 only)
$\kappa$		threshold
	$\kappa_1,\kappa_2$	first and second threshold in deglitch method
$\lambda$		wavelength
	$\lambda_{c}$	central wavelength of filter bandpass
	$\lambda_{ref}$	reference wavelength of filter bandpass
	$\lambda(i)$	centre wavelength of a pixel
$\sigma$		uncertainty or rms
	$\sigma(P)$	uncertainty of detector in-band power in the selected filter band
	$\sigma_{FWHM}$	uncertainty of FWHM
$\Phi$		rotation angle
	$\Phi_{raster}$	raster rotation angle (ATTRROTA)
	$\Phi$	spacecraft roll angle
$\varphi$(i,s(i,t),t)		transfer function converting PHT-S signals s(i,t) to flux densities
$\phi$(t)		orbital phase
$\chi$(i,f)		relative filter-to-filter responsivity correction for detector pixel $i$
	$\chi^{f}$(i)	idem
	$\chi$(f)	idem for a given P detector
$\chi^{2}$		goodness of fit
$\Omega$		solid angle
	$\Omega^{f}_{eff}$	effective solid angle for filter f,