Changeset 1168 in Sophya


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Timestamp:
Aug 31, 2000, 9:42:49 AM (25 years ago)
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ansari
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copie depuis mac - Reza 31/8/2000

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  • trunk/DocHFI_L2/wbsl2.tex

    r1167 r1168  
    5858\item Version 1.1 (April 2000 - CVS version 1.2) \\
    5959Draft updated using the document prepared at ISCTM and IfA (Edinburgh)
    60 \item Version 1.2 (August 2000 - CVS version 1.4) \\
     60\item Version 1.2 (August 2000 - CVS version 1.6) \\
    6161Inclusion of a section describing notation and conventions,
    6262flow charts. A more detailed description of deliverables is also included.
     
    9797\item[]\gph{423}  Polarised TOI processing
    9898\item[]\gph{424}  2-D map reconstruction from TOI's
    99 \item[]\gph{425}  Polarised 2-D map reconstruction from TOI's
     99\item[]\gph{425}  2-D polarisation map reconstruction from TOI's
    100100\item[]\gph{426}  Optimal 2-D map reconstruction and analysis
    101101\item[]\gph{427}  Early Compact Source Catalogue
     
    139139\hline
    140140%               &           &           &       \\
    141 \ngph{421}     &   5     &     \ngph{426}     &   ?     \\
     141\ngph{421}     &    5    &     \ngph{426}     &   ?     \\
    142142%
    143143\ngph{422}     &   15    &     \ngph{427}     &   10     \\
    144144%
    145 \ngph{423}     &   10    &     \ngph{428}     &   30    \\
     145\ngph{423}     &    5    &     \ngph{428}     &   30    \\
    146146%
    147147\ngph{424}     &   15    &     \ngph{429}     &   10    \\
    148148%
    149 \ngph{425}     &   10    &                    &         \\
     149\ngph{425}     &   15    &                    &         \\
    150150%               &           &           &       \\
    151151%
     
    172172\begin{itemize}
    173173\item[] {\bf Coordinates:} The spacecraft attitude is defined by the spin
    174 axis direction $\overrightarrow{\Omega}(\theta, \phi)$.
    175 $\psi$ is the third angle defining the position of the spacecraft
    176 and thus a given detectors view direction and beam pattern orientation.
    177 The spin velocity would be denoted $\omega_z$ or $omega_{\psi}$. \\
     174axis $\overrightarrow{\Omega}$ direction $(\theta, \phi)$ and the
     175roll angle $\psi$. The beam direction and orientation can be computed from
     176the spacecraft attitude ($\overrightarrow{\Omega}, \psi$ using
     177the focal plane geometry.
     178The spin velocity would be denoted $\omega_z$ or $\omega_{\psi}$. \\
    178179A given sky direction is denoted $(\alpha,\delta)$ in equatorial coordinates,
    179180$(l,b)$ in Galactic coordinates or $(\lambda,\beta)$ in ecliptic coordinate.
     
    193194\item[] {\bf Sky map:} The reconstructed signal in a given pixelisation
    194195scheme from a single or a set of detectors. The sky map in a given
    195 frequency channel is denoted $sky(\theta,\phi) \vert ^{\bnu}$.
     196frequency channel is denoted $\boldsymbol{T}^{\bnu}(\theta,\phi)$.
     197$\boldsymbol{I}^{\bnu}$,$\boldsymbol{Q}^{\bnu}$,$\boldsymbol{U}^{\bnu}$ are used
     198for stokes parameters defining the polarisation state.
    196199\end{itemize}
    197200
     
    199202\subsection{Processing steps}
    200203
    201 Unpacking the telemetry packets, uncompressing the science data,
    202 time ordering the data and archiving the data in a format usable
     204The level 2 uses the instrument and spacecraft data obtained
     205from level 1 {\bf DS1} and the instrument calibration data
     206base {\bf DSCal}. calibration data base contains the
     207focal plane geometry, detector response and readout
     208characteristics, beam patterns, filters and polariser
     209response. The main processing steps for HFI-L2 are
     210briefly described here:
     211
     212\begin{itemize}
     213\item {\bf L1:} Unpacking the telemetry packets,
     214uncompressing the science data, time ordering the data and
     215archiving the data in a format usable
    203216by the L2 pipeline is the responsability of Level 1. Detailed
    204217description of L1 software and processing steps is beyond the scope
     
    208221as the auxiliary data (orbit and attitude).
    209222{\bf DS1} is the processed data from level 1 containing the TOI's
    210 (Time Ordered Information).
    211 $$ \boldmath{L1} : \text{DS0} \longrightarrow \text{DS1} $$
    212 
    213 DS1 data set :
    214 \begin{itemize}
    215 \item Raw Time Ordered bolometer signals : $b_{raw}^j(t)$
    216 \item Time Ordered House-keeping data : $HSK(t)$
     223(Time Ordered Information).
     224\begin{center}
     225\framebox{
     226$ \boldmath{L1} : \text{DS0} \longrightarrow \text{DS1} $
     227
     228\end{center}
     229{\bf DS1} data set contains three main components, with different
     230sampling frequency for each component
     231\begin{itemize}
     232\item Raw Time Ordered bolometer signals : $b_{raw}^j(t1)$
     233\item Time Ordered House-keeping data : $HSK(t2)$
     234\item Associated orbit and attitude data : Space craft
     235position $ \boldmath{P}_{xyz}(t3) $, spin axis direction
     236$\overrightarrow{\Omega}(t3) - (\theta, \phi)(t3)$ and the
     237roll angle $\psi(t3)$.
     238\end{itemize}
     239
     240\item {\bf L2-2 , L2-3 :} Cleaning and calibrating the TOI's for
     241non polarised (L2-2) and polarised (L2-3) channels.
     242These processings correspond to \gph{422} and \gph{423}
     243packages.
     244\begin{center}
     245\framebox{
     246$ \boldmath{L2-2} : \text{DS1} \oplus \text{DSCal} \longrightarrow \text{DS2-2} $
     247} (non polarised channels) \\
     248\framebox{
     249$ \boldmath{L2-3} : \text{DS1} \oplus \text{DSCal} \longrightarrow \text{DS2-3} $
     250} (polarised channels)
     251\end{center}
     252In addition to cleaned and calibrated bolometer signals
     253{\bf DS2-2} and {\bf DS2-3} contain data quality flag,
     254the parameters necessary to compute the reconstructed spacecraft
     255orbit and attitude for each time sample, as well as each
     256detector beam pattern direction and orientation.
     257\begin{itemize}
     258\item Cleaned and calibrated Time Ordered bolometer signals : $\bbold_{c}^j(t_1)$
     259\item Data quality flag : $qf_{c}^j(t_1)$
     260\item Reconstructed astrometric calibration parameters \\
     261The pointing direction and beam orientation $(\alpha , \delta)^j(t1) \gamma(t1)$
     262for each detector at any given time can be computed using these parameters.
     263\item Detector response and photometric calibration parameters
     264\item Low frequency drifts and noise statistics
     265\item Reconstructed lobe
     266\item Size reduced TOI's through appropriate processings such as phase
     267binning
     268\item Time Ordered House-keeping data : $HSK(t_2)$
    217269\item Associated orbit and attitude data :
    218 $XYZ(t) , \overrightarrow{\Omega}(t) , \psi(t)$
    219 (spin axis direction $(\theta, \phi)(t)$
    220 \end{itemize}
    221 
    222 {\bf DS0:} Science and House-keeping (HSK) telemetry packets \\
    223 {\bf DS1:} Time ordered - Uncompressed Science data bundeled
    224 with the corresponding house-keeping data. \\
    225 {\bf DS2-2} Cleaned, photometrically calibrated Time ordered data \\
    226 
    227 
     270$\{ \boldmath{P}_{xyz}(t3) , \overrightarrow{\Omega}(t3) , \psi(t3) \} $
     271\end{itemize}
     272
     273\item {\bf L2-4 , L2-5 :} Reconstructing 2-D sky maps using
     274cleaned, calibrated TOI's. The redundancies provided by
     275the scan strategy the sky and the set of detectors in
     276a given frequency channel are used in these steps for assessing
     277and removing the systematic and instrumental effects (low frequency drifts,
     278noise, main lobe and far side lobe effects, \ldots).
     279An iterative, sub-optimal processing method is foreseen for
     280L2-4 and L2-5 (\gph424 and \gph425).
     281\begin{center}
     282\framebox{
     283$ \boldmath{L2-2} : \text{DS2-2} \oplus \text{DSCal} \longrightarrow \text{DS2-4} $
     284} \\
     285\framebox{
     286$ \boldmath{L2-5} : \text{DS2-3} \oplus \text{DSCal} \longrightarrow \text{DS2-5} $
     287}
     288\end{center}
     289Reprocessed TOI's and full sky temperature and polarisation state
     290maps are the main outputs of {\bf L2-4} and {\bf L2-5}:
     291\begin{itemize}
     292\item Reprocessed, calibrated Time Ordered bolometer signals : $\bbold_{rc}^j(t_1)$
     293\item Full sky maps , temperature and polarisation maps (\gph425)
     294$\boldsymbol{I}\bnu (\alpha,\delta)$, $\boldsymbol{Q}\bnu (\alpha,\delta)$,
     295$\boldsymbol{U}\bnu (\alpha,\delta)$.
     296\end{itemize}
     297
     298\item {\bf L2-6} More complex methods for 2-D map reconstruction and
     299data analysis are performed at the next step (\bf L2-6 , \gph426)
     300\begin{center}
     301\framebox{
     302$ \boldmath{L2-6} : \text{DS2-2} \oplus \text{DS2-3} \oplus \text{DSCal} \longrightarrow \text{DS2-6} $
     303}
     304\end{center}
     305
     306\item {\bf L2-7} The Early Compact Source Catalogue (ECSC) is an
     307important data product from HFI Level 2 processing.
     308\begin{center}
     309\framebox{
     310$ \boldmath{L2-7} : \text{DS2-2} \oplus \text{DS2-3} \oplus \text{DSCal} \longrightarrow \text{DS2-7} $ (ECSC)
     311}
     312\end{center}
     313
     314The \bf{DS2-2} and  \bf{DS2-3} are used to produce the source catalogue 
     315containing the source positions, brightness and local
     316sky maps in each frequency bands \bf{DS2-7} :
     317\begin{itemize}
     318\item Source catalogue: $\{ (\alpha,\delta)_i , F_i^{\bnu 1} ,
     319F_i^{\bnu 2} , \ldots \}$
     320\item local sky maps: $\{ lm_i(x,y)^{\bnu 1}, lm_i(x,y)^{\bnu 2}, ldots \}$
     321\end{itemize}
     322
     323\end{itemize}
    228324 
    229325\section{GPH421: RTA/QLA Real Time Assesment, Quick Look Analysis}
     
    231327\item[]\gph{421.1} Quick look analysis
    232328\item[]\gph{421.2} Evaluation of instrument health
    233 \item[]\gph{421.1} Exchange of information with LFI
     329\item[]\gph{421.3} Exchange of information with LFI
    234330of mission/spacecraft/payload-dependent effects common
    235331to both instruments
    236332\end{itemize}
     333
    237334
    238335\section{GPH422: TOI  processing}
     
    298395
    299396\item[]\gph{422.7}  Production of single pointing co-added rings
     397or
    300398 
    301399\item[]\gph{422.9}  Deliverables: Cleaned, calibrated TOI's :
     
    315413in polarised channels.
    316414
    317 \section{GPH424: Simple 2-D map reconstruction}
     415\section{GPH424: 2-D map reconstruction}
    318416
    319417This package contains all the necessary modules for
     
    359457\end{itemize}
    360458
    361 \section{GPH425: Global 2-D map reconstruction}
     459\section{GPH425: 2-D polarisation map reconstruction}
     460The modified version of \gph424 software modules, suitable
     461for processing polarised TOI's for producing polarisation
     462sky maps are grouped in this package.
     463Compared with \gph424 ,
     464\begin{itemize}
     465\item[]\gph{425.9} Deliverables: Full sky polarisation maps \\
     466\begin{itemize}
     467\item Sky maps per frequency channels $map_\nu (\alpha, \delta) $
     468\item Reprocessed TOI's
     469\end{itemize}
     470 
     471\end{itemize}
     472
     473\section{GPH426: Optimal 2-D map reconstruction and analysis}
    362474
    363475Implementation of an optimal 2-D full sky map reconstruction,
     
    368480
    369481\begin{itemize}
     482\item[]\gph{425.1} Optimal 2-D map reconstruction and analysis
     483for non polarised channels
     484\item[]\gph{425.2} Optimal 2-D map reconstruction and analysis
     485for polarised channels
    370486
    371487\item[]\gph{425.9} Deliverables: Full sky maps \\
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