Rename xincl to xinc.

xincl is used to represent the original inclination.
feature/19
Daniel Warner 2018-08-30 14:40:00 +01:00 committed by Daniel Warner
parent 836b67e60c
commit a7d72d70e4
2 changed files with 23 additions and 23 deletions

View File

@ -235,7 +235,7 @@ Eci SGP4::FindPositionSDP4(double tsince) const
double omega;
double xl;
double xnode;
double xincl;
double xinc;
/*
* update for secular gravity and atmospheric drag
@ -254,10 +254,10 @@ Eci SGP4::FindPositionSDP4(double tsince) const
double templ = common_consts_.t2cof * tsq;
double xn = elements_.RecoveredMeanMotion();
e = elements_.Eccentricity();
xincl = elements_.Inclination();
double em = elements_.Eccentricity();
xinc = elements_.Inclination();
DeepSpaceSecular(tsince, xmdf, omgadf, xnode, e, xincl, xn);
DeepSpaceSecular(tsince, xmdf, omgadf, xnode, em, xinc, xn);
if (xn <= 0.0)
{
@ -265,18 +265,18 @@ Eci SGP4::FindPositionSDP4(double tsince) const
}
a = pow(kXKE / xn, kTWOTHIRD) * tempa * tempa;
e -= tempe;
e = em - tempe;
double xmam = xmdf + elements_.RecoveredMeanMotion() * templ;
DeepSpacePeriodics(tsince, e, xincl, omgadf, xnode, xmam);
DeepSpacePeriodics(tsince, e, xinc, omgadf, xnode, xmam);
/*
* keeping xincl positive important unless you need to display xincl
* keeping xinc positive important unless you need to display xinc
* and dislike negative inclinations
*/
if (xincl < 0.0)
if (xinc < 0.0)
{
xincl = -xincl;
xinc = -xinc;
xnode += kPI;
omgadf -= kPI;
}
@ -310,7 +310,7 @@ Eci SGP4::FindPositionSDP4(double tsince) const
double perturbed_x7thm1;
double perturbed_xlcof;
double perturbed_aycof;
RecomputeConstants(xincl,
RecomputeConstants(xinc,
perturbed_sinio,
perturbed_cosio,
perturbed_x3thm1,
@ -328,7 +328,7 @@ Eci SGP4::FindPositionSDP4(double tsince) const
omega,
xl,
xnode,
xincl,
xinc,
perturbed_xlcof,
perturbed_aycof,
perturbed_x3thm1,
@ -338,7 +338,7 @@ Eci SGP4::FindPositionSDP4(double tsince) const
perturbed_sinio);
}
void SGP4::RecomputeConstants(const double xincl,
void SGP4::RecomputeConstants(const double xinc,
double& sinio,
double& cosio,
double& x3thm1,
@ -347,8 +347,8 @@ void SGP4::RecomputeConstants(const double xincl,
double& xlcof,
double& aycof)
{
sinio = sin(xincl);
cosio = cos(xincl);
sinio = sin(xinc);
cosio = cos(xinc);
const double theta2 = cosio * cosio;
@ -378,7 +378,7 @@ Eci SGP4::FindPositionSGP4(double tsince) const
double omega;
double xl;
double xnode;
const double xincl = elements_.Inclination();
const double xinc = elements_.Inclination();
/*
* update for secular gravity and atmospheric drag
@ -451,7 +451,7 @@ Eci SGP4::FindPositionSGP4(double tsince) const
omega,
xl,
xnode,
xincl,
xinc,
common_consts_.xlcof,
common_consts_.aycof,
common_consts_.x3thm1,
@ -468,7 +468,7 @@ Eci SGP4::CalculateFinalPositionVelocity(
const double omega,
const double xl,
const double xnode,
const double xincl,
const double xinc,
const double xlcof,
const double aycof,
const double x3thm1,
@ -600,7 +600,7 @@ Eci SGP4::CalculateFinalPositionVelocity(
+ 0.5 * temp42 * x1mth2 * cos2u;
const double uk = u - 0.25 * temp43 * x7thm1 * sin2u;
const double xnodek = xnode + 1.5 * temp43 * cosio * sin2u;
const double xinck = xincl + 1.5 * temp43 * cosio * sinio * cos2u;
const double xinck = xinc + 1.5 * temp43 * cosio * sinio * cos2u;
const double rdotk = rdot - xn * temp42 * x1mth2 * sin2u;
const double rfdotk = rfdot + xn * temp42 * (x1mth2 * cos2u + 1.5 * x3thm1);
@ -1178,10 +1178,10 @@ void SGP4::DeepSpacePeriodics(
/*
* apply periodics directly
*/
const double tmp_ph = ph / sinis;
ph /= sinis;
omgasm += pgh - cosis * tmp_ph;
xnodes += tmp_ph;
omgasm += pgh - cosis * ph;
xnodes += ph;
xll += pl;
}
else

View File

@ -188,7 +188,7 @@ private:
};
void Initialise();
static void RecomputeConstants(const double xincl,
static void RecomputeConstants(const double xinc,
double& sinio,
double& cosio,
double& x3thm1,
@ -205,7 +205,7 @@ private:
const double omega,
const double xl,
const double xnode,
const double xincl,
const double xinc,
const double xlcof,
const double aycof,
const double x3thm1,