1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 97 98 99 100 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 118 119 120 121 122 123 124 125 126 127 128 129 130 131 132 133 134 135 136 137 138 139 140 141 142 143 144 145 146 147 148 149 150 151 152 153 154 155 156 157 158 159 160 161 162 163 164 165 166 167 168 169 170 171 172 173 174 175 176 177 178 179 180
|
/***********************************************/
/**
* @file observationMiscPodVariational.cpp
*
* @brief Precise Orbit data (variational equations).
*
* @author Torsten Mayer-Guerr
* @date 2015-06-02
*
*/
/***********************************************/
#include "base/import.h"
#include "base/polynomial.h"
#include "files/fileInstrument.h"
#include "misc/observation/variationalEquationFromFile.h"
#include "observationMiscPodVariational.h"
/***********************************************/
ObservationMiscPodVariational::ObservationMiscPodVariational(Config &config)
{
try
{
FileName fileNamePod;
FileName fileNameVariational;
UInt integrationDegree;
renameDeprecatedConfig(config, "representation", "parametrizationGravity", date2time(2020, 6, 3));
renameDeprecatedConfig(config, "parameter", "parametrizationAcceleration", date2time(2020, 6, 3));
if(readConfigSequence(config, "rightHandSide", Config::MUSTSET, "", "input for observation vectors"))
{
readConfig(config, "inputfileOrbit", fileNamePod, Config::MUSTSET, "", "kinematic positions as observations");
endSequence(config);
}
readConfig(config, "inputfileVariational", fileNameVariational, Config::MUSTSET, "", "approximate position and integrated state matrix");
readConfig(config, "ephemerides", ephemerides, Config::OPTIONAL, "jpl", "");
readConfig(config, "parametrizationGravity", parameterGravity, Config::DEFAULT, "", "gravity field parametrization");
readConfig(config, "parametrizationAcceleration", parameterAcceleration, Config::DEFAULT, "", "orbit force parameters");
readConfig(config, "integrationDegree", integrationDegree, Config::DEFAULT, "7", "integration of forces by polynomial approximation of degree n");
readConfig(config, "interpolationDegree", interpolationDegree, Config::DEFAULT, "7", "orbit interpolation by polynomial approximation of degree n");
readConfig(config, "accelerateComputation", accelerateComputation, Config::DEFAULT, "0", "acceleration of computation by transforming the observations");
if(isCreateSchema(config)) return;
// =======================
// init
// ----
podFile.open(fileNamePod);
countArc = podFile.arcCount();
variationalEquation.open(fileNameVariational, parameterGravity, parameterAcceleration, std::vector<Time>(), ephemerides, integrationDegree);
// =======================
// count parameters
// ----------------
countAParameter = variationalEquation.parameterCount();
gravityCount = variationalEquation.parameterCountGravity();
idxGravity = 0;
idxState = gravityCount;
}
catch(std::exception &e)
{
GROOPS_RETHROW(e)
}
}
/***********************************************/
Bool ObservationMiscPodVariational::setInterval(const Time &timeStart, const Time &timeEnd)
{
try
{
Bool change = FALSE;
change = parameterGravity->setInterval(timeStart, timeEnd) || change;
change = parameterAcceleration->setInterval(timeStart, timeEnd) || change;
if(!change)
return FALSE;
variationalEquation.computeIndices();
// count parameters
// ----------------
countAParameter = variationalEquation.parameterCount();
gravityCount = variationalEquation.parameterCountGravity();
idxGravity = 0;
idxState = gravityCount;
return change;
}
catch(std::exception &e)
{
GROOPS_RETHROW(e)
}
}
/***********************************************/
void ObservationMiscPodVariational::parameterName(std::vector<ParameterName> &name) const
{
try
{
variationalEquation.parameterName(name);
}
catch(std::exception &e)
{
GROOPS_RETHROW(e)
}
}
/***********************************************/
ObservationMiscPod::Arc ObservationMiscPodVariational::computeArc(UInt arcNo, CovariancePodPtr covPod)
{
try
{
// read POD observations
// ---------------------
OrbitArc pod = podFile.readArc(arcNo);
const UInt obsCount = 3*pod.size();
if(obsCount == 0)
return Arc();
const std::vector<Time> timePod = pod.times();
VariationalEquationFromFile::ObservationEquation eqn = variationalEquation.integrateArc(timePod.at(0), timePod.back(), TRUE/*position*/, FALSE/*velocity*/);
Polynomial polynomial(eqn.times, interpolationDegree);
// kinematic orbit observations
// ----------------------------
Matrix l(obsCount, 1);
for(UInt k=0; k<obsCount/3; k++)
{
l(3*k+0,0) = pod.at(k).position.x();
l(3*k+1,0) = pod.at(k).position.y();
l(3*k+2,0) = pod.at(k).position.z();
}
l -= polynomial.interpolate(timePod, eqn.pos0, 3);
// =============================================
Matrix A;
if(!accelerateComputation || (l.rows() <= eqn.PosDesign.rows()))
{
// design matrix
// -------------
A = polynomial.interpolate(timePod, eqn.PosDesign, 3);
// decorrelation
// -------------
if(covPod)
covPod->decorrelate(arcNo, pod, {l, A});
}
else
{
A = eqn.PosDesign;
Matrix B = polynomial.interpolate(timePod, identityMatrix(A.rows()), 3);
if(covPod)
covPod->decorrelate(arcNo, pod, {l, B});
const Vector tau = QR_decomposition(B);
QTransMult(B, tau, l);
triangularMult(1., B.row(0, B.columns()), A);
}
// =============================================
Arc observationArc;
observationArc.l = l;
observationArc.A = A;
observationArc.times = timePod;
observationArc.pod = pod;
return observationArc;
}
catch(std::exception &e)
{
GROOPS_RETHROW(e)
}
}
/***********************************************/
|