/**
* @covers Marando\AstroCoord\Frame::FK4
*/
public function testFK4()
{
$equinoxes = [Epoch::B1950(), Epoch::B1900(), Epoch::B(1948), Epoch::dt(AstroDate::now())];
foreach ($equinoxes as $e) {
$equinox = $e;
$fk4 = Frame::FK4($e);
$this->assertEquals('FK4', $fk4->name);
$this->assertEquals($equinox, $fk4->equinox);
}
}
public function testToEclip()
{
// Earth -> Venus @ 2015-Nov-08 23:20:34.000 UT
$dt = AstroDate::jd(2457335.47261574);
$x = Distance::au(-0.7956853147170494);
$y = Distance::au(-0.00807301690301796);
$z = Distance::au(0.01392567642390632);
$c = new Cartesian(Frame::ICRF(), $dt->toEpoch(), $x, $y, $z);
$equat = $c->toEquat();
$eclip = $equat->toEclip();
$prec = Angle::arcmin(13)->deg;
$this->assertEquals(180.3510658, $eclip->lon->deg, 'λ', $prec);
$this->assertEquals(1.1487465, $eclip->lat->deg, 'β', $prec);
}
public function test()
{
return;
$frame = Frame::ICRF();
$epoch = Epoch::J(2000);
echo $epoch->toDate()->toTDB();
echo "\n";
echo "\n";
exit;
$ra = \Marando\Units\Time::hms(11, 16, 46.6);
$dec = \Marando\Units\Angle::dms(5, 45, 32.5);
$dist = Distance::au(5.8);
echo "\n" . ($eq = new Equat($frame, $epoch, $ra, $dec, $dist));
echo "\n" . ($eq = (new Equat($frame, $epoch, $ra, $dec, $dist))->apparent());
echo "\n";
return;
$frame = Frame::ICRF();
$epoch = AstroDate::jd(2457335.472615741)->toEpoch();
$ra = \Marando\Units\Time::hms(11, 16, 46.6);
$dec = \Marando\Units\Angle::dms(5, 45, 32.5);
$dist = Distance::au(5.8);
echo "\n" . ($eq = new Equat($frame, $epoch, $ra, $dec, $dist));
echo "\n" . ($eq = (new Equat($frame, $epoch, $ra, $dec, $dist))->apparent());
$eq = new Equat($frame, $epoch, $ra, $dec, $dist);
$eq->topo = Geo::deg(27, -82);
echo "\n" . $eq->toHoriz();
echo "\n" . $eq->apparent();
echo "\n" . ($h = $eq->toHoriz());
echo "\n" . $h->az->deg . "\t" . $h->alt->deg;
echo "\n" . $eq->apparent(\Marando\Units\Pressure::mbar(100), \Marando\Units\Temperature::F(90), 0.85);
echo "\n" . $eq->toHoriz();
return;
$ra = \Marando\Units\Time::hours(14.424354);
$dec = \Marando\Units\Angle::deg(33.54366);
$dist = Distance::au(1.5);
$geo = Geo::deg(27, -82);
$e = new Equat(Frame::ICRF(), Epoch::jd(2455586), $ra, $dec, $dist);
$e->topo = $geo;
echo "\n\n" . $e;
echo "\n" . $e->apparent();
$e = new Equat(Frame::ICRF(), Epoch::jd(2455586), $ra, $dec, $dist);
$e->topo = $geo;
echo "\n" . $e->apparent();
$e = new Equat(Frame::ICRF(), Epoch::jd(2455586), $ra, $dec, $dist);
$e->topo = $geo;
echo "\n" . $e->toHoriz();
return;
$e = new Equat(Frame::ICRF(), Epoch::jd(2455586), $ra, $dec, $dist);
echo "\n\n" . $e;
echo "\n" . $e->apparent($geo);
echo "\n" . $e->apparent()->toHoriz($geo);
$e = new Equat(Frame::ICRF(), Epoch::jd(2455586), $ra, $dec, $dist);
echo "\n\n" . $e;
echo "\n" . $e->apparent();
echo "\n" . $e->apparent()->toHoriz();
$e = new Equat(Frame::ICRF(), Epoch::jd(2451586), $ra, $dec, $dist);
$e->topo = $geo;
echo "\n\n" . $e;
echo "\n" . $e->apparent();
echo "\n" . $e->apparent()->toHoriz();
return;
// Position of Mercury
$x = Distance::au(+1.18052679326447);
$y = Distance::au(-0.3650485652522116);
$z = Distance::au(-0.2123422968928603);
// Velocity of Mercury
$vx = Velocity::aud(0.02052320553396918);
$vy = Velocity::aud(0.02828864020900079);
$vz = Velocity::aud(0.01145246106968459);
// Frame & epoch
$frame = Frame::ICRF();
$epoch = AstroDate::parse('2015-Mar-20')->toEpoch();
$c = new Cartesian($frame, $epoch, $x, $y, $z, $vx, $vy, $vz);
echo "\n\n";
echo $c;
echo "\n\n";
echo $c->setUnit('km km/d');
echo "\n\n";
echo $c->setUnit('km km/s');
echo "\n\n";
echo $c->toEquat();
echo "\n\n";
echo $c->toEquat()->apparent();
echo "\n\n";
echo $c->toEquat()->apparent(Geo::deg(27, 278));
echo "\n\n";
echo $c->toEquat()->toHoriz(Geo::deg(27, 278));
echo "\n\n";
}
public function testCreateWithAstroDate()
{
$x = Distance::au(+9.32);
$y = Distance::au(-5.25);
$z = Distance::au(-6.89);
$c = new Cartesian(Frame::ICRF(), AstroDate::now(), $x, $y, $z);
}
