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315 lines (263 loc) · 12.5 KB
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function MARSIS_postgis_ingest_orbit(orbit_id, ingest_data, ingest_sim, ingest_meta)
tic
if (nargin<4) error("NOT enough input arguments"); end
RdrDir = '../../MARSIS_data_l2';
EdrSimDir = '../../MARSIS_sim';
MARSIS_DATA_COLLECTION = 'MARSIS_dataP';
MARSIS_META_COLLECTION = 'MARSIS_echo_meta';
%%%% DATA and METADATA files %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
if (orbit_id<9999)
EdrSimFile = ['E_0',num2str(orbit_id),'_SS3_TRK_CMP_M_SIM.DAT'];
RdrFile = ['R_0',num2str(orbit_id),'_SS3_TRK_CMP_M.DAT'];
else
EdrSimFile = ['E_', num2str(orbit_id),'_SS3_TRK_CMP_M_SIM.DAT'];
RdrFile = ['R_', num2str(orbit_id),'_SS3_TRK_CMP_M.DAT'];
end
if (EdrSimDir==0) EdrSimDir = DefEdrSimDir; end
if (RdrDir==0) RdrDir = DefRdrDir; end
EdrSimFile = fullfile(EdrSimDir,EdrSimFile);
RdrFile = fullfile(RdrDir,RdrFile);
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
if ingest_data
%%% Reading DATA from RDR file %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
ECHO_MODULUS_MINUS1_F1_DIP = read_MARSIS_RDR( RdrFile, 'ECHO_MODULUS_MINUS1_F1_DIP' );
ECHO_PHASE_MINUS1_F1_DIP = read_MARSIS_RDR( RdrFile, 'ECHO_PHASE_MINUS1_F1_DIP' );
ECHO_MODULUS_ZERO_F1_DIP = read_MARSIS_RDR( RdrFile, 'ECHO_MODULUS_ZERO_F1_DIP' );
ECHO_PHASE_ZERO_F1_DIP = read_MARSIS_RDR( RdrFile, 'ECHO_PHASE_ZERO_F1_DIP' );
ECHO_MODULUS_PLUS1_F1_DIP = read_MARSIS_RDR( RdrFile, 'ECHO_MODULUS_PLUS1_F1_DIP' );
ECHO_PHASE_PLUS1_F1_DIP = read_MARSIS_RDR( RdrFile, 'ECHO_PHASE_PLUS1_F1_DIP' );
ECHO_MODULUS_MINUS1_F2_DIP = read_MARSIS_RDR( RdrFile, 'ECHO_MODULUS_MINUS1_F2_DIP' );
ECHO_PHASE_MINUS1_F2_DIP = read_MARSIS_RDR( RdrFile, 'ECHO_PHASE_MINUS1_F2_DIP' );
ECHO_MODULUS_ZERO_F2_DIP = read_MARSIS_RDR( RdrFile, 'ECHO_MODULUS_ZERO_F2_DIP' );
ECHO_PHASE_ZERO_F2_DIP = read_MARSIS_RDR( RdrFile, 'ECHO_PHASE_ZERO_F2_DIP' );
ECHO_MODULUS_PLUS1_F2_DIP = read_MARSIS_RDR( RdrFile, 'ECHO_MODULUS_PLUS1_F2_DIP' );
ECHO_PHASE_PLUS1_F2_DIP = read_MARSIS_RDR( RdrFile, 'ECHO_PHASE_PLUS1_F2_DIP' );
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
data = [ECHO_MODULUS_MINUS1_F1_DIP ...
ECHO_PHASE_MINUS1_F1_DIP ...
ECHO_MODULUS_ZERO_F1_DIP ...
ECHO_PHASE_ZERO_F1_DIP ...
ECHO_MODULUS_PLUS1_F1_DIP ...
ECHO_PHASE_PLUS1_F1_DIP ...
ECHO_MODULUS_MINUS1_F2_DIP ...
ECHO_PHASE_MINUS1_F2_DIP ...
ECHO_MODULUS_ZERO_F2_DIP ...
ECHO_PHASE_ZERO_F2_DIP ...
ECHO_MODULUS_PLUS1_F2_DIP ...
ECHO_PHASE_PLUS1_F2_DIP];
[N_samples, N_echoes] = size(ECHO_MODULUS_MINUS1_F1_DIP);
end
%%% Reading SIMULATIONS from EDR ISM file %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
#EdrSimFile ="../../MARSIS_sim/E_01886_SS3_TRK_CMP_M_SIM.DAT"; # altrimenti non trova la sim. Per mettere i adti senza sim.
if ingest_sim
[ ~, ~, ~, ~, scetfw, ~, ~, ~, ~, x0, y0, z0, alt0, ~, ~, ~, ~, ~, esm1f1, es00f1, esp1f1, esm1f2, es00f2, esp1f2 ] = readmarsisedrsim( EdrSimFile );
[N_samples, N_echoes] = size(esm1f1);
################################################################
B = 1e6; % bandwidth
fs = 1.4e6; % echo sampling frequency
Ns = 512; % number of echo samples
[ ~ , f ] = fftvars( fs, Ns );
[ iband ] = find( abs( f ) <= B/2 );
fband = f( iband );
Nf = length( fband );
frames = length( scetfw );
% window = ones( size( f ) );
window = zeros( size( f ) );
% window( iband ) = ifftshift( hamming( Nf ) );
window( iband ) = ifftshift( hanning( Nf ) );
window = reshape( window, Ns, 1 ) * ones( 1, frames );
esm1f1 = window .* esm1f1;
es00f1 = window .* es00f1;
esp1f1 = window .* esp1f1;
esm1f2 = window .* esm1f2;
es00f2 = window .* es00f2;
esp1f2 = window .* esp1f2;
r_s_max = 3417500; % reference distance of echoes from the center of Mars
c = 299792458; % Velocity of light in vacuo in m/s
alt_max = 25e3; % reference altitude over the Martian ellipsoid
positn = [ x0; y0; z0 ];
r = sqrt( x0.^2 + y0.^2 + z0.^2 );
% [ ~, alt0 ] = cspice_nearpt( positn, a, a, b );
deltat = 2 * ( r_s_max - r + alt0 - alt_max ) / c;
[ deltat, f ] = meshgrid( deltat, f );
phase = exp( 2 .* 1i .* pi .* deltat .* f );
esm1f1 = phase .* esm1f1;
es00f1 = phase .* es00f1;
esp1f1 = phase .* esp1f1;
esm1f2 = phase .* esm1f2;
es00f2 = phase .* es00f2;
esp1f2 = phase .* esp1f2;
em1f1 = ifft( esm1f1 );
e00f1 = ifft( es00f1 );
ep1f1 = ifft( esp1f1 );
em1f2 = ifft( esm1f2 );
e00f2 = ifft( es00f2 );
ep1f2 = ifft( esp1f2 );
% mola = molaset( lon_0, lat_0, 'radius', 128 );
wm1f1 = 20 * log10( abs( em1f1 ) );
w00f1 = 20 * log10( abs( e00f1 ) );
wp1f1 = 20 * log10( abs( ep1f1 ) );
wm1f2 = 20 * log10( abs( em1f2 ) );
w00f2 = 20 * log10( abs( e00f2 ) );
wp1f2 = 20 * log10( abs( ep1f2 ) );
bwimage = [ wm1f1,wm1f1, w00f1,w00f1, wp1f1,wp1f1, wm1f2,wm1f2, w00f2,w00f2, wp1f2,wp1f2 ];
dynrange = 65;
maxbwimage = max( max( bwimage ) );
bwimage( bwimage < maxbwimage - dynrange ) = maxbwimage - dynrange;
bwimage = (rescale2d( bwimage, 0, 300 ))+1;
################################################################
#sim_cmp = [esm1f1, es00f1, esp1f1, esm1f2, es00f2, esp1f2];
#sim_cmp = [wm1f1, w00f1, wp1f1, wm1f2, w00f2, wp1f2];
#sim_r = real(sim_cmp);
#sim_i = imag(sim_cmp);
#sim = [sim_r, sim_i];
#size(bwimage)
#size(data)
#imwrite(double(data),'test.jpg');
max(max(data))
min(min(data))
max(max(bwimage))
min(min(bwimage))
#return;
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
end
if ingest_meta
%%% Reading METADATA from RDR file %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
CENTRAL_FREQUENCY = read_MARSIS_RDR( RdrFile, 'CENTRAL_FREQUENCY' );
SLOPE = read_MARSIS_RDR( RdrFile, 'SLOPE' );
SCET_FRAME_WHOLE = read_MARSIS_RDR( RdrFile, 'SCET_FRAME_WHOLE' );
SCET_FRAME_FRAC = read_MARSIS_RDR( RdrFile, 'SCET_FRAME_FRAC' );
H_SCET_PAR = read_MARSIS_RDR( RdrFile, 'H_SCET_PAR' );
VT_SCET_PAR = read_MARSIS_RDR( RdrFile, 'VT_SCET_PAR' );
VR_SCET_PAR = read_MARSIS_RDR( RdrFile, 'VR_SCET_PAR' );
DELTA_S_SCET_PAR = read_MARSIS_RDR( RdrFile, 'DELTA_S_SCET_PAR' );
NA_SCET_PAR = read_MARSIS_RDR( RdrFile, 'NA_SCET_PAR' );
GEOMETRY_EPHEMERIS_TIME = read_MARSIS_RDR( RdrFile, 'GEOMETRY_EPHEMERIS_TIME' );
GEOMETRY_EPOCH = read_MARSIS_RDR( RdrFile, 'GEOMETRY_EPOCH' );
MARS_SOLAR_LONGITUDE = read_MARSIS_RDR( RdrFile, 'MARS_SOLAR_LONGITUDE' );
MARS_SUN_DISTANCE = read_MARSIS_RDR( RdrFile, 'MARS_SUN_DISTANCE' );
ORBIT_NUMBER = read_MARSIS_RDR( RdrFile, 'ORBIT_NUMBER' );
TARGET_NAME = read_MARSIS_RDR( RdrFile, 'TARGET_NAME' );
TARGET_SC_POSITION_VECTOR = read_MARSIS_RDR( RdrFile, 'TARGET_SC_POSITION_VECTOR' );
SPACECRAFT_ALTITUDE = read_MARSIS_RDR( RdrFile, 'SPACECRAFT_ALTITUDE' );
SUB_SC_LONGITUDE = read_MARSIS_RDR( RdrFile, 'SUB_SC_LONGITUDE' );
SUB_SC_LATITUDE = read_MARSIS_RDR( RdrFile, 'SUB_SC_LATITUDE' );
TARGET_SC_VELOCITY_VECTOR = read_MARSIS_RDR( RdrFile, 'TARGET_SC_VELOCITY_VECTOR' );
TARGET_SC_RADIAL_VELOCITY = read_MARSIS_RDR( RdrFile, 'TARGET_SC_RADIAL_VELOCITY' );
TARGET_SC_TANG_VELOCITY = read_MARSIS_RDR( RdrFile, 'TARGET_SC_TANG_VELOCITY' );
LOCAL_TRUE_SOLAR_TIME = read_MARSIS_RDR( RdrFile, 'LOCAL_TRUE_SOLAR_TIME' );
SOLAR_ZENITH_ANGLE = read_MARSIS_RDR( RdrFile, 'SOLAR_ZENITH_ANGLE' );
DIPOLE_UNIT_VECTOR = read_MARSIS_RDR( RdrFile, 'DIPOLE_UNIT_VECTOR' );
MONOPOLE_UNIT_VECTOR = read_MARSIS_RDR( RdrFile, 'MONOPOLE_UNIT_VECTOR' );
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
end
%meta = [CENTRAL_FREQUENCY(1) ...
% CENTRAL_FREQUENCY(2) ...
% SLOPE ...
% SCET_FRAME_WHOLE ...
% SCET_FRAME_FRAC ...
% H_SCET_PAR ...
% VT_SCET_PAR ...
% VR_SCET_PAR ...
% DELTA_S_SCET_PAR ...
% NA_SCET_PAR(1) ...
% NA_SCET_PAR(2) ...
% GEOMETRY_EPHEMERIS_TIME ...
% MARS_SOLAR_LONGITUDE ...
% MARS_SUN_DISTANCE ...
% ORBIT_NUMBER ...
% TARGET_NAME(1) ...
% TARGET_SC_POSITION_VECTOR(1) ...
% TARGET_SC_POSITION_VECTOR(2) ...
% TARGET_SC_POSITION_VECTOR(3) ...
% SPACECRAFT_ALTITUDE ...
% SUB_SC_LONGITUDE ...
% SUB_SC_LATITUDE ...
% TARGET_SC_VELOCITY_VECTOR(1) ...
% TARGET_SC_VELOCITY_VECTOR(2) ...
% TARGET_SC_VELOCITY_VECTOR(3) ...
% TARGET_SC_RADIAL_VELOCITY ...
% TARGET_SC_TANG_VELOCITY ...
% LOCAL_TRUE_SOLAR_TIME ...
% SOLAR_ZENITH_ANGLE ...
% DIPOLE_UNIT_VECTOR(1) ...
% DIPOLE_UNIT_VECTOR(2) ...
% DIPOLE_UNIT_VECTOR(3) ...
% MONOPOLE_UNIT_VECTOR(1) ...
% MONOPOLE_UNIT_VECTOR(2) ...
% MONOPOLE_UNIT_VECTOR(3)];
if ingest_data
MARSIS_DATA_COLLECTION = 'data';
COLLECTION_TYPE_DATA = 'MARSIS_data_cubeSO';
ARRAY_0 = '[0:0, 0:0, 0:0]';
VALUE_0_DATA='{0f,0f,0f,0f,0f,0f,0f,0f,0f,0f,0f,0f}';
create_collection_string = ["rasql -q 'create collection MARSIS_" MARSIS_DATA_COLLECTION "_" num2str(orbit_id) " " COLLECTION_TYPE_DATA "' --user rasadmin --passwd rasadmin"];
system(create_collection_string);
init_collection_string = ["rasql -q 'insert into MARSIS_" MARSIS_DATA_COLLECTION "_" num2str(orbit_id) " values marray " COLLECTION_TYPE_DATA " in [0:" num2str(N_echoes) ",0:" num2str(N_samples) "] values " VALUE_0_DATA "' --user rasadmin --passwd rasadmin"];
system(init_collection_string);
end
if ingest_sim
%%% SIMULATiONS
MARSIS_CSCS_COLLECTION = 'cscs';
COLLECTION_TYPE_CSCS = COLLECTION_TYPE_DATA; %'MARSIS_cscs_cubeSO';
VALUE_0_CSCS=VALUE_0_DATA;%'{0d,0d,0d,0d,0d,0d,0d,0d,0d,0d,0d,0d}';
create_collection_string = ["rasql -q 'create collection MARSIS_" MARSIS_CSCS_COLLECTION "_" num2str(orbit_id) " " COLLECTION_TYPE_CSCS "' --user rasadmin --passwd rasadmin"];
system(create_collection_string);
init_collection_string = ["rasql -q 'insert into MARSIS_" MARSIS_CSCS_COLLECTION "_" num2str(orbit_id) " values marray " COLLECTION_TYPE_CSCS " in [0:" num2str(N_echoes) ",0:" num2str(N_samples) "] values " VALUE_0_CSCS "' --user rasadmin --passwd rasadmin"];
system(init_collection_string);
end
#return;
for ii = 1:N_echoes
if ingest_meta
printf("%d\n",ii);
fflush(stdout);
meta.orbit_id = ORBIT_NUMBER(ii);
meta.echo_id = ii;
meta.sub_sc_lon = SUB_SC_LONGITUDE(ii);
meta.sub_sc_lat = SUB_SC_LATITUDE(ii);
meta.f1 = CENTRAL_FREQUENCY(1,ii);
meta.f2 = CENTRAL_FREQUENCY(2,ii);
meta.slope = SLOPE(ii);
meta.scet_frame_w = SCET_FRAME_WHOLE(ii);
meta.scet_frame_f = SCET_FRAME_FRAC(ii);
meta.h_scet = H_SCET_PAR(ii);
meta.vt_scet = VT_SCET_PAR(ii);
meta.vr_scet = VR_SCET_PAR(ii);
meta.delta_s_scet = DELTA_S_SCET_PAR(ii);
meta.na_scet_1 = NA_SCET_PAR(1,ii);
meta.na_scet_2 = NA_SCET_PAR(2,ii);
meta.geom_ephem_t = GEOMETRY_EPHEMERIS_TIME(ii);
meta.geom_epoch_utc = GEOMETRY_EPOCH(:,ii)';
meta.solar_lon = MARS_SOLAR_LONGITUDE(ii);
meta.mars_sun_dist = MARS_SUN_DISTANCE(ii);
meta.target_name = TARGET_NAME(:,ii)';
meta.target_sc_pos_x = TARGET_SC_POSITION_VECTOR(1,ii);
meta.target_sc_pos_y = TARGET_SC_POSITION_VECTOR(2,ii);
meta.target_sc_pos_z = TARGET_SC_POSITION_VECTOR(3,ii);
meta.sc_alt = SPACECRAFT_ALTITUDE(ii);
meta.target_sc_vel_x = TARGET_SC_VELOCITY_VECTOR(1,ii);
meta.target_sc_vel_y = TARGET_SC_VELOCITY_VECTOR(2,ii);
meta.target_sc_vel_z = TARGET_SC_VELOCITY_VECTOR(3,ii);
meta.target_sc_rad_v = TARGET_SC_RADIAL_VELOCITY(ii);
meta.target_sc_tan_v = TARGET_SC_TANG_VELOCITY(ii);
meta.loc_solar_t = LOCAL_TRUE_SOLAR_TIME(ii);
meta.solar_zen = SOLAR_ZENITH_ANGLE(ii);
meta.di_uni_x = DIPOLE_UNIT_VECTOR(1,ii);
meta.di_uni_y = DIPOLE_UNIT_VECTOR(2,ii);
meta.di_uni_z = DIPOLE_UNIT_VECTOR(3,ii);
meta.mono_uni_x = MONOPOLE_UNIT_VECTOR(1,ii);
meta.mono_uni_y = MONOPOLE_UNIT_VECTOR(2,ii);
meta.mono_uni_z = MONOPOLE_UNIT_VECTOR(3,ii);
% META
MARSIS_postgis_ingest_echo_meta(meta,"marsis_echoes_meta");
end
if ingest_data
% DATA
MARSIS_rasda_ingest_echo_data_so(data(:,ii:N_echoes:end),orbit_id,meta.echo_id,["MARSIS_" MARSIS_DATA_COLLECTION "_" num2str(orbit_id)]);
end
if ingest_sim
% SIM
MARSIS_rasda_ingest_echo_data_so( bwimage(:,ii:N_echoes:end),orbit_id,meta.echo_id,["MARSIS_" MARSIS_CSCS_COLLECTION "_" num2str(orbit_id)]);
end
end
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