| /dports/astro/gpstk/GPSTk-8.0.0/core/tests/GNSSEph/ |
| H A D | dump2code.pl | 46 my ($prn, $health, $tocStr, $toeStr, $af0, $af1, $af2, $A, $Adot, $dn, $dndot,
91 $dndot = $arr[4];
139 printf(" oe.dndot = $dndot;\n");
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| H A D | GPSEphemerisStore_T.cpp | 135 eph1.dndot = 0; in doGetPrnXvtTests()
174 eph2.dndot = 0; in doGetPrnXvtTests()
213 eph3.dndot = 0; in doGetPrnXvtTests()
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| H A D | BDSEphemeris_T.cpp | 84 oe.dndot = 0; in testSvXvtMEO()
204 oe.dndot = 0.00000000E+00; in testSvXvtGEO()
318 oe.dndot = 0.00000000E+00;
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| H A D | OrbitEph_T.cpp | 75 oe.dndot = 0; in testSvXvt()
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| H A D | OrbElem_T.cpp | 91 oe.dndot = 0; in testSvXvt()
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| H A D | BrcKeplerOrbit_T.cpp | 122 TUASSERTE(double, 0, empty.dndot); in initializationTest()
241 orbitCopy.dndot = 2.8e-12; in equalityTest()
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| /dports/astro/gpstk/GPSTk-8.0.0/core/lib/GNSSEph/ |
| H A D | OrbElem.cpp | 61 dn(0.0), dndot(0.0), ecc(0.0), A(0.0), Adot(0.0), OMEGA0(0.0), in OrbElem()
93 if (dndot != right->dndot) return false; in isSameData()
120 if (dndot != right->dndot) retList.push_back("dndot"); in compare()
232 double dnA = dn + 0.5 * dndot * elapte; in svXvt()
371 double dnA = dn + 0.5 * dndot * elapte; in svRelativity()
508 << setw(fw) << dndot << " rad/(sec**2)" << endl in dumpBody()
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| H A D | BrcKeplerOrbit.cpp | 65 Cuc = Cus = Crc = Crs = Cic = Cis = M0 = dn = dndot = in BrcKeplerOrbit()
121 (dndot == right.dndot) && in operator ==()
169 dndot = dndotArg; in loadData()
272 dndot = 0.0; in loadData()
702 return dndot; in getDnDot()
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| H A D | EngEphemeris.cpp | 1067 double dndot = 0.0; in loadData() local
1091 m0, Dn, dndot, Ecc, A, ahalf, Adot, Omega0, I0, W, in loadData()
1206 double dndot = 0.0; in setSF2() local
1234 dndot, Ecc, A, ahalf, Adot, Omega0, I0, W, OmegaDot, in setSF2()
1284 double dndot = 0.0; in setSF3() local
1297 dndot = orbit.getDnDot(); in setSF3()
1322 dndot, Ecc, A, ahalf, Adot, Omega0, I0, W, OmegaDot, in setSF3()
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| H A D | OrbElem.hpp | 196 double dndot; /**< Rate of correction to mean motion (rad/sec/sec) */ member in gpstk::OrbElem
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| H A D | OrbitEph.hpp | 212 double dndot; ///< Rate of correction to mean motion (rad/sec/sec) member in gpstk::OrbitEph
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| H A D | BrcKeplerOrbit.hpp | 378 double dndot; /**< Rate of correction to mean motion (rad/sec/sec) */ member in gpstk::BrcKeplerOrbit
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| H A D | OrbitEph.cpp | 70 dndot(0.0), Adot(0.0), in OrbitEph()
154 double dnA = dn + 0.5*dndot*elapte; in svXvt()
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| H A D | OrbElemRinex.cpp | 237 dndot = 0.0; in loadData()
320 dndot = 0.0; in loadData()
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| /dports/astro/gpstk/GPSTk-8.0.0/core/lib/FileHandling/RINEX3/ |
| H A D | Rinex3NavData.cpp | 597 double dndot = 0.0; in operator EngEphemeris() local
624 M0, dn, dndot, ecc, A, Ahalf, Adot, OMEGA0, i0, in operator EngEphemeris()
672 oeptr->dndot = 0.; in castTo()
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| /dports/astro/gpstk/GPSTk-8.0.0/core/lib/FileHandling/RINEX/ |
| H A D | RinexNavData.cpp | 214 gpse.dndot = 0.; in operator GPSEphemeris()
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| /dports/science/code_saturne/code_saturne-7.1.0/tests/ |
| H A D | cs_blas_test.c | 1659 dndot(n, 1, y, 1, 1, da, 1, 1, x, 1, 1); in _ad_x_test()
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