geocent.cpp

projapi是一个关于GIS行业投影转换的程序库

#include "stdafx.h"
#include "geocent.h"
#include <math.h>
/*
 *    math.h     - is needed for calls to sin, cos, tan and sqrt.
 *    geocent.h  - is needed for Error codes and prototype error checking.
 */


/***************************************************************************/
/*
 *                               DEFINES
 */
#define PI         3.14159265358979323e0
#define PI_OVER_2  (PI / 2.0e0)
#define FALSE      0
#define TRUE       1
#define COS_67P5   0.38268343236508977  /* cosine of 67.5 degrees */
#define AD_C       1.0026000            /* Toms region 1 constant */


/***************************************************************************/
/*
 *                              GLOBAL DECLARATIONS
 */
/* Ellipsoid parameters, default to WGS 84 */
double Geocent_a = 6378137.0;     /* Semi-major axis of ellipsoid in meters */
double Geocent_b = 6356752.3142;  /* Semi-minor axis of ellipsoid           */

double Geocent_a2 = 40680631590769.0;        /* Square of semi-major axis */
double Geocent_b2 = 40408299984087.05;       /* Square of semi-minor axis */
double Geocent_e2 = 0.0066943799901413800;   /* Eccentricity squared  */
double Geocent_ep2 = 0.00673949675658690300; /* 2nd eccentricity squared */
/*
 * These state variables are for optimization purposes.  The only function
 * that should modify them is Set_Geocentric_Parameters.
 */


/***************************************************************************/
/*
 *                              FUNCTIONS     
 */


long Set_Geocentric_Parameters (double a, 
                                double b) 
{ /* BEGIN Set_Geocentric_Parameters */
/*
 * The function Set_Geocentric_Parameters receives the ellipsoid parameters
 * as inputs and sets the corresponding state variables.
 *
 *    a  : Semi-major axis, in meters.          (input)
 *    b  : Semi-minor axis, in meters.          (input)
 */
  long Error_Code = GEOCENT_NO_ERROR;

  if (a <= 0.0)
    Error_Code |= GEOCENT_A_ERROR;
  if (b <= 0.0)
    Error_Code |= GEOCENT_B_ERROR;
  if (a < b)
    Error_Code |= GEOCENT_A_LESS_B_ERROR;
  if (!Error_Code)
  {
    Geocent_a = a;
    Geocent_b = b;
    Geocent_a2 = a * a;
    Geocent_b2 = b * b;
    Geocent_e2 = (Geocent_a2 - Geocent_b2) / Geocent_a2;
    Geocent_ep2 = (Geocent_a2 - Geocent_b2) / Geocent_b2;
  }
  return (Error_Code);
} /* END OF Set_Geocentric_Parameters */


void Get_Geocentric_Parameters (double *a, 
                                double *b)
{ /* BEGIN Get_Geocentric_Parameters */
/*
 * The function Get_Geocentric_Parameters returns the ellipsoid parameters
 * to be used in geocentric coordinate conversions.
 *
 *    a  : Semi-major axis, in meters.          (output)
 *    b  : Semi-minor axis, in meters.          (output)
 */

  *a = Geocent_a;
  *b = Geocent_b;
} /* END OF Get_Geocentric_Parameters */


long Convert_Geodetic_To_Geocentric (double Latitude,
                                     double Longitude,
                                     double Height,
                                     double *X,
                                     double *Y,
                                     double *Z) 
{ /* BEGIN Convert_Geodetic_To_Geocentric */
/*
 * The function Convert_Geodetic_To_Geocentric converts geodetic coordinates
 * (latitude, longitude, and height) to geocentric coordinates (X, Y, Z),
 * according to the current ellipsoid parameters.
 *
 *    Latitude  : Geodetic latitude in radians                     (input)
 *    Longitude : Geodetic longitude in radians                    (input)
 *    Height    : Geodetic height, in meters                       (input)
 *    X         : Calculated Geocentric X coordinate, in meters    (output)
 *    Y         : Calculated Geocentric Y coordinate, in meters    (output)
 *    Z         : Calculated Geocentric Z coordinate, in meters    (output)
 *
 */
  long Error_Code = GEOCENT_NO_ERROR;
  double Rn;            /*  Earth radius at location  */
  double Sin_Lat;       /*  sin(Latitude)  */
  double Sin2_Lat;      /*  Square of sin(Latitude)  */
  double Cos_Lat;       /*  cos(Latitude)  */

  /*
  ** Don't blow up if Latitude is just a little out of the value
  ** range as it may just be a rounding issue.  Also removed longitude
  ** test, it should be wrapped by cos() and sin().  NFW for PROJ.4, Sep/2001.
  */
  if( Latitude < -PI_OVER_2 && Latitude > -1.001 * PI_OVER_2 )
      Latitude = -PI_OVER_2;
  else if( Latitude > PI_OVER_2 && Latitude < 1.001 * PI_OVER_2 )
      Latitude = PI_OVER_2;
  else if ((Latitude < -PI_OVER_2) || (Latitude > PI_OVER_2))
  { /* Latitude out of range */
    Error_Code |= GEOCENT_LAT_ERROR;
  }

  if (!Error_Code)
  { /* no errors */
    if (Longitude > PI)
      Longitude -= (2*PI);
    Sin_Lat = sin(Latitude);
    Cos_Lat = cos(Latitude);
    Sin2_Lat = Sin_Lat * Sin_Lat;
    Rn = Geocent_a / (sqrt(1.0e0 - Geocent_e2 * Sin2_Lat));
    *X = (Rn + Height) * Cos_Lat * cos(Longitude);
    *Y = (Rn + Height) * Cos_Lat * sin(Longitude);
    *Z = ((Rn * (1 - Geocent_e2)) + Height) * Sin_Lat;

  }
  return (Error_Code);
} /* END OF Convert_Geodetic_To_Geocentric */

/*
 * The function Convert_Geocentric_To_Geodetic converts geocentric
 * coordinates (X, Y, Z) to geodetic coordinates (latitude, longitude, 
 * and height), according to the current ellipsoid parameters.
 *
 *    X         : Geocentric X coordinate, in meters.         (input)
 *    Y         : Geocentric Y coordinate, in meters.         (input)
 *    Z         : Geocentric Z coordinate, in meters.         (input)
 *    Latitude  : Calculated latitude value in radians.       (output)
 *    Longitude : Calculated longitude value in radians.      (output)
 *    Height    : Calculated height value, in meters.         (output)
 */

#define USE_ITERATIVE_METHOD

void Convert_Geocentric_To_Geodetic (double X,
                                     double Y, 
                                     double Z,
                                     double *Latitude,
                                     double *Longitude,
                                     double *Height)
{ /* BEGIN Convert_Geocentric_To_Geodetic */
#if !defined(USE_ITERATIVE_METHOD)
/*
 * The method used here is derived from 'An Improved Algorithm for
 * Geocentric to Geodetic Coordinate Conversion', by Ralph Toms, Feb 1996
 */

/* Note: Variable names follow the notation used in Toms, Feb 1996 */

    double W;        /* distance from Z axis */
    double W2;       /* square of distance from Z axis */
    double T0;       /* initial estimate of vertical component */
    double T1;       /* corrected estimate of vertical component */
    double S0;       /* initial estimate of horizontal component */
    double S1;       /* corrected estimate of horizontal component */
    double Sin_B0;   /* sin(B0), B0 is estimate of Bowring aux variable */
    double Sin3_B0;  /* cube of sin(B0) */
    double Cos_B0;   /* cos(B0) */
    double Sin_p1;   /* sin(phi1), phi1 is estimated latitude */
    double Cos_p1;   /* cos(phi1) */
    double Rn;       /* Earth radius at location */
    double Sum;      /* numerator of cos(phi1) */
    int At_Pole;     /* indicates location is in polar region */

    At_Pole = FALSE;
    if (X != 0.0)
    {
        *Longitude = atan2(Y,X);
    }
    else
    {
        if (Y > 0)
        {
            *Longitude = PI_OVER_2;
        }
        else if (Y < 0)
        {
            *Longitude = -PI_OVER_2;
        }
        else
        {
            At_Pole = TRUE;
            *Longitude = 0.0;
            if (Z > 0.0)
            {  /* north pole */
                *Latitude = PI_OVER_2;
            }
            else if (Z < 0.0)
            {  /* south pole */
                *Latitude = -PI_OVER_2;
            }
            else
            {  /* center of earth */
                *Latitude = PI_OVER_2;
                *Height = -Geocent_b;
                return;
            } 
        }
    }
    W2 = X*X + Y*Y;
    W = sqrt(W2);
    T0 = Z * AD_C;
    S0 = sqrt(T0 * T0 + W2);
    Sin_B0 = T0 / S0;
    Cos_B0 = W / S0;
    Sin3_B0 = Sin_B0 * Sin_B0 * Sin_B0;
    T1 = Z + Geocent_b * Geocent_ep2 * Sin3_B0;
    Sum = W - Geocent_a * Geocent_e2 * Cos_B0 * Cos_B0 * Cos_B0;
    S1 = sqrt(T1*T1 + Sum * Sum);
    Sin_p1 = T1 / S1;
    Cos_p1 = Sum / S1;
    Rn = Geocent_a / sqrt(1.0 - Geocent_e2 * Sin_p1 * Sin_p1);
    if (Cos_p1 >= COS_67P5)
    {
        *Height = W / Cos_p1 - Rn;
    }
    else if (Cos_p1 <= -COS_67P5)
    {
        *Height = W / -Cos_p1 - Rn;
    }
    else
    {
        *Height = Z / Sin_p1 + Rn * (Geocent_e2 - 1.0);
    }
    if (At_Pole == FALSE)
    {
        *Latitude = atan(Sin_p1 / Cos_p1);
    }
#else /* defined(USE_ITERATIVE_METHOD) */
/*
* Reference...
* ============
* Wenzel, H.-G.(1985): Hochauflösende Kugelfunktionsmodelle für
* das Gravitationspotential der Erde. Wiss. Arb. Univ. Hannover
* Nr. 137, p. 130-131.

* Programmed by GGA- Leibniz-Institue of Applied Geophysics
*               Stilleweg 2
*               D-30655 Hannover
*               Federal Republic of Germany
*               Internet: www.gga-hannover.de
*
*               Hannover, March 1999, April 2004.
*               see also: comments in statements
* remarks:
* Mathematically exact and because of symmetry of rotation-ellipsoid,
* each point (X,Y,Z) has at least two solutions (Latitude1,Longitude1,Height1) and
* (Latitude2,Longitude2,Height2). Is point=(0.,0.,Z) (P=0.), so you get even
* four solutions,	every two symmetrical to the semi-minor axis.
* Here Height1 and Height2 have at least a difference in order of
* radius of curvature (e.g. (0,0,b)=> (90.,0.,0.) or (-90.,0.,-2b);
* (a+100.)*(sqrt(2.)/2.,sqrt(2.)/2.,0.) => (0.,45.,100.) or
* (0.,225.,-(2a+100.))).
* The algorithm always computes (Latitude,Longitude) with smallest |Height|.
* For normal computations, that means |Height|<10000.m, algorithm normally
* converges after to 2-3 steps!!!
* But if |Height| has the amount of length of ellipsoid's axis
* (e.g. -6300000.m),	algorithm needs about 15 steps.
*/

/* local defintions and variables */
/* end-criterium of loop, accuracy of sin(Latitude) */
#define genau   1.E-12
#define genau2  (genau*genau)
#define maxiter 30

    double P;        /* distance between semi-minor axis and location */
    double RR;       /* distance between center and location */
    double CT;       /* sin of geocentric latitude */
    double ST;       /* cos of geocentric latitude */
    double RX;
    double RK;
    double RN;       /* Earth radius at location */
    double CPHI0;    /* cos of start or old geodetic latitude in iterations */
    double SPHI0;    /* sin of start or old geodetic latitude in iterations */
    double CPHI;     /* cos of searched geodetic latitude */
    double SPHI;     /* sin of searched geodetic latitude */
    double SDPHI;    /* end-criterium: addition-theorem of sin(Latitude(iter)-Latitude(iter-1)) */
    int At_Pole;     /* indicates location is in polar region */
    int iter;        /* # of continous iteration, max. 30 is always enough (s.a.) */

    At_Pole = FALSE;
    P = sqrt(X*X+Y*Y);
    RR = sqrt(X*X+Y*Y+Z*Z);

/*	special cases for latitude and longitude */
    if (P/Geocent_a < genau) {

/*  special case, if P=0. (X=0., Y=0.) */
        At_Pole = TRUE;
	*Longitude = 0.;

/*  if (X,Y,Z)=(0.,0.,0.) then Height becomes semi-minor axis
 *  of ellipsoid (=center of mass), Latitude becomes PI/2 */
        if (RR/Geocent_a < genau) {
            *Latitude = PI_OVER_2;
            *Height   = -Geocent_b;
            return ;

        }
    }
    else {
/*  ellipsoidal (geodetic) longitude
 *  interval: -PI < Longitude <= +PI */
        *Longitude=atan2(Y,X);
    }

/* --------------------------------------------------------------
 * Following iterative algorithm was developped by
 * "Institut für Erdmessung", University of Hannover, July 1988.
 * Internet: www.ife.uni-hannover.de
 * Iterative computation of CPHI,SPHI and Height.
 * Iteration of CPHI and SPHI to 10**-12 radian resp.
 * 2*10**-7 arcsec.
 * --------------------------------------------------------------
 */
    CT = Z/RR;
    ST = P/RR;
    RX = 1.0/sqrt(1.0-Geocent_e2*(2.0-Geocent_e2)*ST*ST);
    CPHI0 = ST*(1.0-Geocent_e2)*RX;
    SPHI0 = CT*RX;
    iter = 0;

/* loop to find sin(Latitude) resp. Latitude
 * until |sin(Latitude(iter)-Latitude(iter-1))| < genau */
    do
    {
        iter++;
        RN = Geocent_a/sqrt(1.0-Geocent_e2*SPHI0*SPHI0);

/*  ellipsoidal (geodetic) height */
        *Height = P*CPHI0+Z*SPHI0-RN*(1.0-Geocent_e2*SPHI0*SPHI0);

        RK = Geocent_e2*RN/(RN+*Height);
        RX = 1.0/sqrt(1.0-RK*(2.0-RK)*ST*ST);
        CPHI = ST*(1.0-RK)*RX;
        SPHI = CT*RX;
        SDPHI = SPHI*CPHI0-CPHI*SPHI0;
        CPHI0 = CPHI;
        SPHI0 = SPHI;
    }
    while (SDPHI*SDPHI > genau2 && iter < maxiter);

/*	ellipsoidal (geodetic) latitude */
    *Latitude=atan(SPHI/fabs(CPHI));

    return;
#endif /* defined(USE_ITERATIVE_METHOD) */
} /* END OF Convert_Geocentric_To_Geodetic */