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1173 lines
36 KiB
C
1173 lines
36 KiB
C
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/////////////////////////////////////////////
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// Solar Position Algorithm (SPA) //
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// for //
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// Solar Radiation Application //
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// //
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// May 12, 2003 //
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// //
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// Filename: SPA.C //
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// //
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// Afshin Michael Andreas //
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// Afshin.Andreas@NREL.gov (303)384-6383 //
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// //
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// Metrology Laboratory //
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// Solar Radiation Research Laboratory //
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// National Renewable Energy Laboratory //
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// 15013 Denver W Pkwy, Golden, CO 80401 //
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/////////////////////////////////////////////
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/////////////////////////////////////////////
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// See the SPA.H header file for usage //
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// //
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// This code is based on the NREL //
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// technical report "Solar Position //
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// Algorithm for Solar Radiation //
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// Application" by I. Reda & A. Andreas //
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/////////////////////////////////////////////
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///////////////////////////////////////////////////////////////////////////////////////////////
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//
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// NOTICE
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// Copyright (C) 2008-2011 Alliance for Sustainable Energy, LLC, All Rights Reserved
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//
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//The Solar Position Algorithm ("Software") is code in development prepared by employees of the
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//Alliance for Sustainable Energy, LLC, (hereinafter the "Contractor"), under Contract No.
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//DE-AC36-08GO28308 ("Contract") with the U.S. Department of Energy (the "DOE"). The United
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//States Government has been granted for itself and others acting on its behalf a paid-up, non-
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//exclusive, irrevocable, worldwide license in the Software to reproduce, prepare derivative
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//works, and perform publicly and display publicly. Beginning five (5) years after the date
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//permission to assert copyright is obtained from the DOE, and subject to any subsequent five
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//(5) year renewals, the United States Government is granted for itself and others acting on
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//its behalf a paid-up, non-exclusive, irrevocable, worldwide license in the Software to
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//reproduce, prepare derivative works, distribute copies to the public, perform publicly and
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//display publicly, and to permit others to do so. If the Contractor ceases to make this
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//computer software available, it may be obtained from DOE's Office of Scientific and Technical
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//Information's Energy Science and Technology Software Center (ESTSC) at P.O. Box 1020, Oak
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//Ridge, TN 37831-1020. THIS SOFTWARE IS PROVIDED BY THE CONTRACTOR "AS IS" AND ANY EXPRESS OR
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//IMPLIED WARRANTIES, INCLUDING BUT NOT LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY
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//AND FITNESS FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE CONTRACTOR OR THE
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//U.S. GOVERNMENT BE LIABLE FOR ANY SPECIAL, INDIRECT OR CONSEQUENTIAL DAMAGES OR ANY DAMAGES
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//WHATSOEVER, INCLUDING BUT NOT LIMITED TO CLAIMS ASSOCIATED WITH THE LOSS OF DATA OR PROFITS,
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//WHICH MAY RESULT FROM AN ACTION IN CONTRACT, NEGLIGENCE OR OTHER TORTIOUS CLAIM THAT ARISES
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//OUT OF OR IN CONNECTION WITH THE ACCESS, USE OR PERFORMANCE OF THIS SOFTWARE.
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//
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//The Software is being provided for internal, noncommercial purposes only and shall not be
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//re-distributed. Please contact the NREL Commercialization and Technology Transfer Office
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//for information concerning a commercial license to use the Software, visit:
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//http://midcdmz.nrel.gov/spa/ for the contact information.
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//
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//As a condition of using the Software in an application, the developer of the application
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//agrees to reference the use of the Software and make this Notice readily accessible to any
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//end-user in a Help|About screen or equivalent manner.
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//
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///////////////////////////////////////////////////////////////////////////////////////////////
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///////////////////////////////////////////////////////////////////////////////////////////////
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// Revised 27-FEB-2004 Andreas
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// Added bounds check on inputs and return value for spa_calculate().
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// Revised 10-MAY-2004 Andreas
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// Changed temperature bound check minimum from -273.15 to -273 degrees C.
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// Revised 17-JUN-2004 Andreas
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// Corrected a problem that caused a bogus sunrise/set/transit on the equinox.
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// Revised 18-JUN-2004 Andreas
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// Added a "function" input variable that allows the selecting of desired outputs.
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// Revised 21-JUN-2004 Andreas
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// Added 3 new intermediate output values to SPA structure (srha, ssha, & sta).
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// Revised 23-JUN-2004 Andreas
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// Enumerations for "function" were renamed and 2 were added.
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// Prevented bound checks on inputs that are not used (based on function).
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// Revised 01-SEP-2004 Andreas
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// Changed a local variable from integer to double.
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// Revised 12-JUL-2005 Andreas
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// Put a limit on the EOT calculation, so that the result is between -20 and 20.
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// Revised 26-OCT-2005 Andreas
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// Set the atmos. refraction correction to zero, when sun is below horizon.
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// Made atmos_refract input a requirement for all "functions".
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// Changed atmos_refract bound check from +/- 10 to +/- 5 degrees.
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// Revised 07-NOV-2006 Andreas
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// Corrected 3 earth periodic terms in the L_TERMS array.
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// Corrected 2 earth periodic terms in the R_TERMS array.
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// Revised 10-NOV-2006 Andreas
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// Corrected a constant used to calculate topocentric sun declination.
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// Put a limit on observer hour angle, so result is between 0 and 360.
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// Revised 13-NOV-2006 Andreas
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// Corrected calculation of topocentric sun declination.
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// Converted all floating point inputs in spa structure to doubles.
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// Revised 27-FEB-2007 Andreas
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// Minor correction made as to when atmos. refraction correction is set to zero.
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// Revised 21-JAN-2008 Andreas
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// Minor change to two variable declarations.
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// Revised 12-JAN-2009 Andreas
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// Changed timezone bound check from +/-12 to +/-18 hours.
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// Revised 14-JAN-2009 Andreas
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// Corrected a constant used to calculate ecliptic mean obliquity.
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// Revised 01-APR-2013 Andreas
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// Replace floor with new integer function for tech. report consistency, no affect on results.
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// Add "utility" function prototypes to header file for use with NREL's SAMPA.
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// Rename 4 "utility" function names (remove "sun") for clarity with NREL's SAMPA.
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// Added delta_ut1 as required input, which the fractional second difference between UT and UTC.
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// Time must be input w/o delta_ut1 adjustment, instead of assuming adjustment was pre-applied.
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// Revised 10-JUL-2014 Andreas
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// Change second in spa_data structure from an integer to double to allow fractional second
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// Revised 08-SEP-2014 Andreas
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// Corrected description of azm_rotation in header file
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// Limited azimuth180 to range of 0 to 360 deg (instead of -180 to 180) for tech report consistency
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// Changed all variables names from azimuth180 to azimuth_astro
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// Renamed 2 "utility" function names for consistency
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///////////////////////////////////////////////////////////////////////////////////////////////
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#include <math.h>
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#include "spa.h"
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#define PI 3.1415926535897932384626433832795028841971
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#define SUN_RADIUS 0.26667
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#define L_COUNT 6
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#define B_COUNT 2
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#define R_COUNT 5
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#define Y_COUNT 63
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#define L_MAX_SUBCOUNT 64
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#define B_MAX_SUBCOUNT 5
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#define R_MAX_SUBCOUNT 40
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enum {TERM_A, TERM_B, TERM_C, TERM_COUNT};
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enum {TERM_X0, TERM_X1, TERM_X2, TERM_X3, TERM_X4, TERM_X_COUNT};
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enum {TERM_PSI_A, TERM_PSI_B, TERM_EPS_C, TERM_EPS_D, TERM_PE_COUNT};
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enum {JD_MINUS, JD_ZERO, JD_PLUS, JD_COUNT};
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enum {SUN_TRANSIT, SUN_RISE, SUN_SET, SUN_COUNT};
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#define TERM_Y_COUNT TERM_X_COUNT
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const int l_subcount[L_COUNT] = {64,34,20,7,3,1};
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const int b_subcount[B_COUNT] = {5,2};
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const int r_subcount[R_COUNT] = {40,10,6,2,1};
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///////////////////////////////////////////////////
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/// Earth Periodic Terms
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///////////////////////////////////////////////////
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const double L_TERMS[L_COUNT][L_MAX_SUBCOUNT][TERM_COUNT]=
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{
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{
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{175347046.0,0,0},
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{3341656.0,4.6692568,6283.07585},
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{34894.0,4.6261,12566.1517},
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{3497.0,2.7441,5753.3849},
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{3418.0,2.8289,3.5231},
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{3136.0,3.6277,77713.7715},
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{2676.0,4.4181,7860.4194},
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{2343.0,6.1352,3930.2097},
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{1324.0,0.7425,11506.7698},
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{1273.0,2.0371,529.691},
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{1199.0,1.1096,1577.3435},
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{990,5.233,5884.927},
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{902,2.045,26.298},
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{857,3.508,398.149},
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{780,1.179,5223.694},
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{753,2.533,5507.553},
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{505,4.583,18849.228},
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{492,4.205,775.523},
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{357,2.92,0.067},
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{317,5.849,11790.629},
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{284,1.899,796.298},
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{271,0.315,10977.079},
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{243,0.345,5486.778},
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{206,4.806,2544.314},
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{205,1.869,5573.143},
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{202,2.458,6069.777},
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{156,0.833,213.299},
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{132,3.411,2942.463},
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{126,1.083,20.775},
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{115,0.645,0.98},
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{103,0.636,4694.003},
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{102,0.976,15720.839},
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{102,4.267,7.114},
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{99,6.21,2146.17},
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{98,0.68,155.42},
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{86,5.98,161000.69},
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{85,1.3,6275.96},
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{85,3.67,71430.7},
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{80,1.81,17260.15},
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{79,3.04,12036.46},
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{75,1.76,5088.63},
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{74,3.5,3154.69},
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{74,4.68,801.82},
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{70,0.83,9437.76},
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{62,3.98,8827.39},
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{61,1.82,7084.9},
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{57,2.78,6286.6},
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{56,4.39,14143.5},
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{56,3.47,6279.55},
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{52,0.19,12139.55},
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{52,1.33,1748.02},
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{51,0.28,5856.48},
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{49,0.49,1194.45},
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{41,5.37,8429.24},
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{41,2.4,19651.05},
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{39,6.17,10447.39},
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{37,6.04,10213.29},
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{37,2.57,1059.38},
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{36,1.71,2352.87},
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{36,1.78,6812.77},
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{33,0.59,17789.85},
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{30,0.44,83996.85},
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{30,2.74,1349.87},
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{25,3.16,4690.48}
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},
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{
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{628331966747.0,0,0},
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{206059.0,2.678235,6283.07585},
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{4303.0,2.6351,12566.1517},
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{425.0,1.59,3.523},
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{119.0,5.796,26.298},
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{109.0,2.966,1577.344},
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{93,2.59,18849.23},
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{72,1.14,529.69},
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{68,1.87,398.15},
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{67,4.41,5507.55},
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{59,2.89,5223.69},
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{56,2.17,155.42},
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{45,0.4,796.3},
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{36,0.47,775.52},
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{29,2.65,7.11},
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{21,5.34,0.98},
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{19,1.85,5486.78},
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{19,4.97,213.3},
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{17,2.99,6275.96},
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{16,0.03,2544.31},
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{16,1.43,2146.17},
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{15,1.21,10977.08},
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{12,2.83,1748.02},
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{12,3.26,5088.63},
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{12,5.27,1194.45},
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{12,2.08,4694},
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{11,0.77,553.57},
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{10,1.3,6286.6},
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{10,4.24,1349.87},
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{9,2.7,242.73},
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{9,5.64,951.72},
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{8,5.3,2352.87},
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{6,2.65,9437.76},
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{6,4.67,4690.48}
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},
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{
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{52919.0,0,0},
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{8720.0,1.0721,6283.0758},
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{309.0,0.867,12566.152},
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{27,0.05,3.52},
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{16,5.19,26.3},
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{16,3.68,155.42},
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{10,0.76,18849.23},
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{9,2.06,77713.77},
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{7,0.83,775.52},
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{5,4.66,1577.34},
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{4,1.03,7.11},
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{4,3.44,5573.14},
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{3,5.14,796.3},
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{3,6.05,5507.55},
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{3,1.19,242.73},
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{3,6.12,529.69},
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{3,0.31,398.15},
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{3,2.28,553.57},
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{2,4.38,5223.69},
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{2,3.75,0.98}
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},
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{
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{289.0,5.844,6283.076},
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{35,0,0},
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{17,5.49,12566.15},
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{3,5.2,155.42},
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{1,4.72,3.52},
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{1,5.3,18849.23},
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{1,5.97,242.73}
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},
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{
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{114.0,3.142,0},
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{8,4.13,6283.08},
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{1,3.84,12566.15}
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},
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{
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{1,3.14,0}
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}
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};
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const double B_TERMS[B_COUNT][B_MAX_SUBCOUNT][TERM_COUNT]=
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{
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{
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{280.0,3.199,84334.662},
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{102.0,5.422,5507.553},
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{80,3.88,5223.69},
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{44,3.7,2352.87},
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{32,4,1577.34}
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},
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{
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{9,3.9,5507.55},
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{6,1.73,5223.69}
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}
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};
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const double R_TERMS[R_COUNT][R_MAX_SUBCOUNT][TERM_COUNT]=
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{
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{
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{100013989.0,0,0},
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{1670700.0,3.0984635,6283.07585},
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{13956.0,3.05525,12566.1517},
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{3084.0,5.1985,77713.7715},
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{1628.0,1.1739,5753.3849},
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{1576.0,2.8469,7860.4194},
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{925.0,5.453,11506.77},
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{542.0,4.564,3930.21},
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{472.0,3.661,5884.927},
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{346.0,0.964,5507.553},
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{329.0,5.9,5223.694},
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{307.0,0.299,5573.143},
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{243.0,4.273,11790.629},
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{212.0,5.847,1577.344},
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{186.0,5.022,10977.079},
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{175.0,3.012,18849.228},
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{110.0,5.055,5486.778},
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{98,0.89,6069.78},
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{86,5.69,15720.84},
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{86,1.27,161000.69},
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{65,0.27,17260.15},
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{63,0.92,529.69},
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{57,2.01,83996.85},
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{56,5.24,71430.7},
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{49,3.25,2544.31},
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{47,2.58,775.52},
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{45,5.54,9437.76},
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{43,6.01,6275.96},
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{39,5.36,4694},
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{38,2.39,8827.39},
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{37,0.83,19651.05},
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{37,4.9,12139.55},
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{36,1.67,12036.46},
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{35,1.84,2942.46},
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{33,0.24,7084.9},
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{32,0.18,5088.63},
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{32,1.78,398.15},
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{28,1.21,6286.6},
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{28,1.9,6279.55},
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{26,4.59,10447.39}
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},
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{
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{103019.0,1.10749,6283.07585},
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{1721.0,1.0644,12566.1517},
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{702.0,3.142,0},
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{32,1.02,18849.23},
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{31,2.84,5507.55},
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{25,1.32,5223.69},
|
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{18,1.42,1577.34},
|
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{10,5.91,10977.08},
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{9,1.42,6275.96},
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{9,0.27,5486.78}
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},
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{
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{4359.0,5.7846,6283.0758},
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{124.0,5.579,12566.152},
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{12,3.14,0},
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{9,3.63,77713.77},
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{6,1.87,5573.14},
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{3,5.47,18849.23}
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},
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{
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{145.0,4.273,6283.076},
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{7,3.92,12566.15}
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},
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{
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{4,2.56,6283.08}
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}
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};
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////////////////////////////////////////////////////////////////
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/// Periodic Terms for the nutation in longitude and obliquity
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////////////////////////////////////////////////////////////////
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const int Y_TERMS[Y_COUNT][TERM_Y_COUNT]=
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{
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{0,0,0,0,1},
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{-2,0,0,2,2},
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{0,0,0,2,2},
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{0,0,0,0,2},
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{0,1,0,0,0},
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{0,0,1,0,0},
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{-2,1,0,2,2},
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{0,0,0,2,1},
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{0,0,1,2,2},
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{-2,-1,0,2,2},
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{-2,0,1,0,0},
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{-2,0,0,2,1},
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{0,0,-1,2,2},
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{2,0,0,0,0},
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{0,0,1,0,1},
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{2,0,-1,2,2},
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{0,0,-1,0,1},
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{0,0,1,2,1},
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{-2,0,2,0,0},
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{0,0,-2,2,1},
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{2,0,0,2,2},
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{0,0,2,2,2},
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{0,0,2,0,0},
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{-2,0,1,2,2},
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{0,0,0,2,0},
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{-2,0,0,2,0},
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{0,0,-1,2,1},
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{0,2,0,0,0},
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{2,0,-1,0,1},
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{-2,2,0,2,2},
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{0,1,0,0,1},
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{-2,0,1,0,1},
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{0,-1,0,0,1},
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{0,0,2,-2,0},
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{2,0,-1,2,1},
|
|
{2,0,1,2,2},
|
|
{0,1,0,2,2},
|
|
{-2,1,1,0,0},
|
|
{0,-1,0,2,2},
|
|
{2,0,0,2,1},
|
|
{2,0,1,0,0},
|
|
{-2,0,2,2,2},
|
|
{-2,0,1,2,1},
|
|
{2,0,-2,0,1},
|
|
{2,0,0,0,1},
|
|
{0,-1,1,0,0},
|
|
{-2,-1,0,2,1},
|
|
{-2,0,0,0,1},
|
|
{0,0,2,2,1},
|
|
{-2,0,2,0,1},
|
|
{-2,1,0,2,1},
|
|
{0,0,1,-2,0},
|
|
{-1,0,1,0,0},
|
|
{-2,1,0,0,0},
|
|
{1,0,0,0,0},
|
|
{0,0,1,2,0},
|
|
{0,0,-2,2,2},
|
|
{-1,-1,1,0,0},
|
|
{0,1,1,0,0},
|
|
{0,-1,1,2,2},
|
|
{2,-1,-1,2,2},
|
|
{0,0,3,2,2},
|
|
{2,-1,0,2,2},
|
|
};
|
|
|
|
const double PE_TERMS[Y_COUNT][TERM_PE_COUNT]={
|
|
{-171996,-174.2,92025,8.9},
|
|
{-13187,-1.6,5736,-3.1},
|
|
{-2274,-0.2,977,-0.5},
|
|
{2062,0.2,-895,0.5},
|
|
{1426,-3.4,54,-0.1},
|
|
{712,0.1,-7,0},
|
|
{-517,1.2,224,-0.6},
|
|
{-386,-0.4,200,0},
|
|
{-301,0,129,-0.1},
|
|
{217,-0.5,-95,0.3},
|
|
{-158,0,0,0},
|
|
{129,0.1,-70,0},
|
|
{123,0,-53,0},
|
|
{63,0,0,0},
|
|
{63,0.1,-33,0},
|
|
{-59,0,26,0},
|
|
{-58,-0.1,32,0},
|
|
{-51,0,27,0},
|
|
{48,0,0,0},
|
|
{46,0,-24,0},
|
|
{-38,0,16,0},
|
|
{-31,0,13,0},
|
|
{29,0,0,0},
|
|
{29,0,-12,0},
|
|
{26,0,0,0},
|
|
{-22,0,0,0},
|
|
{21,0,-10,0},
|
|
{17,-0.1,0,0},
|
|
{16,0,-8,0},
|
|
{-16,0.1,7,0},
|
|
{-15,0,9,0},
|
|
{-13,0,7,0},
|
|
{-12,0,6,0},
|
|
{11,0,0,0},
|
|
{-10,0,5,0},
|
|
{-8,0,3,0},
|
|
{7,0,-3,0},
|
|
{-7,0,0,0},
|
|
{-7,0,3,0},
|
|
{-7,0,3,0},
|
|
{6,0,0,0},
|
|
{6,0,-3,0},
|
|
{6,0,-3,0},
|
|
{-6,0,3,0},
|
|
{-6,0,3,0},
|
|
{5,0,0,0},
|
|
{-5,0,3,0},
|
|
{-5,0,3,0},
|
|
{-5,0,3,0},
|
|
{4,0,0,0},
|
|
{4,0,0,0},
|
|
{4,0,0,0},
|
|
{-4,0,0,0},
|
|
{-4,0,0,0},
|
|
{-4,0,0,0},
|
|
{3,0,0,0},
|
|
{-3,0,0,0},
|
|
{-3,0,0,0},
|
|
{-3,0,0,0},
|
|
{-3,0,0,0},
|
|
{-3,0,0,0},
|
|
{-3,0,0,0},
|
|
{-3,0,0,0},
|
|
};
|
|
|
|
///////////////////////////////////////////////
|
|
|
|
double rad2deg(double radians)
|
|
{
|
|
return (180.0/PI)*radians;
|
|
}
|
|
|
|
double deg2rad(double degrees)
|
|
{
|
|
return (PI/180.0)*degrees;
|
|
}
|
|
|
|
int integer(double value)
|
|
{
|
|
return value;
|
|
}
|
|
|
|
double limit_degrees(double degrees)
|
|
{
|
|
double limited;
|
|
|
|
degrees /= 360.0;
|
|
limited = 360.0*(degrees-floor(degrees));
|
|
if (limited < 0) limited += 360.0;
|
|
|
|
return limited;
|
|
}
|
|
|
|
double limit_degrees180pm(double degrees)
|
|
{
|
|
double limited;
|
|
|
|
degrees /= 360.0;
|
|
limited = 360.0*(degrees-floor(degrees));
|
|
if (limited < -180.0) limited += 360.0;
|
|
else if (limited > 180.0) limited -= 360.0;
|
|
|
|
return limited;
|
|
}
|
|
|
|
double limit_degrees180(double degrees)
|
|
{
|
|
double limited;
|
|
|
|
degrees /= 180.0;
|
|
limited = 180.0*(degrees-floor(degrees));
|
|
if (limited < 0) limited += 180.0;
|
|
|
|
return limited;
|
|
}
|
|
|
|
double limit_zero2one(double value)
|
|
{
|
|
double limited;
|
|
|
|
limited = value - floor(value);
|
|
if (limited < 0) limited += 1.0;
|
|
|
|
return limited;
|
|
}
|
|
|
|
double limit_minutes(double minutes)
|
|
{
|
|
double limited=minutes;
|
|
|
|
if (limited < -20.0) limited += 1440.0;
|
|
else if (limited > 20.0) limited -= 1440.0;
|
|
|
|
return limited;
|
|
}
|
|
|
|
double dayfrac_to_local_hr(double dayfrac, double timezone)
|
|
{
|
|
return 24.0*limit_zero2one(dayfrac + timezone/24.0);
|
|
}
|
|
|
|
double third_order_polynomial(double a, double b, double c, double d, double x)
|
|
{
|
|
return ((a*x + b)*x + c)*x + d;
|
|
}
|
|
|
|
///////////////////////////////////////////////////////////////////////////////////////////////
|
|
int validate_inputs(spa_data *spa)
|
|
{
|
|
if ((spa->year < -2000) || (spa->year > 6000)) return 1;
|
|
if ((spa->month < 1 ) || (spa->month > 12 )) return 2;
|
|
if ((spa->day < 1 ) || (spa->day > 31 )) return 3;
|
|
if ((spa->hour < 0 ) || (spa->hour > 24 )) return 4;
|
|
if ((spa->minute < 0 ) || (spa->minute > 59 )) return 5;
|
|
if ((spa->second < 0 ) || (spa->second >=60 )) return 6;
|
|
if ((spa->pressure < 0 ) || (spa->pressure > 5000)) return 12;
|
|
if ((spa->temperature <= -273) || (spa->temperature > 6000)) return 13;
|
|
if ((spa->delta_ut1 <= -1 ) || (spa->delta_ut1 >= 1 )) return 17;
|
|
if ((spa->hour == 24 ) && (spa->minute > 0 )) return 5;
|
|
if ((spa->hour == 24 ) && (spa->second > 0 )) return 6;
|
|
|
|
if (fabs(spa->delta_t) > 8000 ) return 7;
|
|
if (fabs(spa->timezone) > 18 ) return 8;
|
|
if (fabs(spa->longitude) > 180 ) return 9;
|
|
if (fabs(spa->latitude) > 90 ) return 10;
|
|
if (fabs(spa->atmos_refract) > 5 ) return 16;
|
|
if ( spa->elevation < -6500000) return 11;
|
|
|
|
if ((spa->function == SPA_ZA_INC) || (spa->function == SPA_ALL))
|
|
{
|
|
if (fabs(spa->slope) > 360) return 14;
|
|
if (fabs(spa->azm_rotation) > 360) return 15;
|
|
}
|
|
|
|
return 0;
|
|
}
|
|
///////////////////////////////////////////////////////////////////////////////////////////////
|
|
double julian_day (int year, int month, int day, int hour, int minute, double second, double dut1, double tz)
|
|
{
|
|
double day_decimal, julian_day, a;
|
|
|
|
day_decimal = day + (hour - tz + (minute + (second + dut1)/60.0)/60.0)/24.0;
|
|
|
|
if (month < 3) {
|
|
month += 12;
|
|
year--;
|
|
}
|
|
|
|
julian_day = integer(365.25*(year+4716.0)) + integer(30.6001*(month+1)) + day_decimal - 1524.5;
|
|
|
|
if (julian_day > 2299160.0) {
|
|
a = integer(year/100);
|
|
julian_day += (2 - a + integer(a/4));
|
|
}
|
|
|
|
return julian_day;
|
|
}
|
|
|
|
double julian_century(double jd)
|
|
{
|
|
return (jd-2451545.0)/36525.0;
|
|
}
|
|
|
|
double julian_ephemeris_day(double jd, double delta_t)
|
|
{
|
|
return jd+delta_t/86400.0;
|
|
}
|
|
|
|
double julian_ephemeris_century(double jde)
|
|
{
|
|
return (jde - 2451545.0)/36525.0;
|
|
}
|
|
|
|
double julian_ephemeris_millennium(double jce)
|
|
{
|
|
return (jce/10.0);
|
|
}
|
|
|
|
double earth_periodic_term_summation(const double terms[][TERM_COUNT], int count, double jme)
|
|
{
|
|
int i;
|
|
double sum=0;
|
|
|
|
for (i = 0; i < count; i++)
|
|
sum += terms[i][TERM_A]*cos(terms[i][TERM_B]+terms[i][TERM_C]*jme);
|
|
|
|
return sum;
|
|
}
|
|
|
|
double earth_values(double term_sum[], int count, double jme)
|
|
{
|
|
int i;
|
|
double sum=0;
|
|
|
|
for (i = 0; i < count; i++)
|
|
sum += term_sum[i]*pow(jme, i);
|
|
|
|
sum /= 1.0e8;
|
|
|
|
return sum;
|
|
}
|
|
|
|
double earth_heliocentric_longitude(double jme)
|
|
{
|
|
double sum[L_COUNT];
|
|
int i;
|
|
|
|
for (i = 0; i < L_COUNT; i++)
|
|
sum[i] = earth_periodic_term_summation(L_TERMS[i], l_subcount[i], jme);
|
|
|
|
return limit_degrees(rad2deg(earth_values(sum, L_COUNT, jme)));
|
|
|
|
}
|
|
|
|
double earth_heliocentric_latitude(double jme)
|
|
{
|
|
double sum[B_COUNT];
|
|
int i;
|
|
|
|
for (i = 0; i < B_COUNT; i++)
|
|
sum[i] = earth_periodic_term_summation(B_TERMS[i], b_subcount[i], jme);
|
|
|
|
return rad2deg(earth_values(sum, B_COUNT, jme));
|
|
|
|
}
|
|
|
|
double earth_radius_vector(double jme)
|
|
{
|
|
double sum[R_COUNT];
|
|
int i;
|
|
|
|
for (i = 0; i < R_COUNT; i++)
|
|
sum[i] = earth_periodic_term_summation(R_TERMS[i], r_subcount[i], jme);
|
|
|
|
return earth_values(sum, R_COUNT, jme);
|
|
|
|
}
|
|
|
|
double geocentric_longitude(double l)
|
|
{
|
|
double theta = l + 180.0;
|
|
|
|
if (theta >= 360.0) theta -= 360.0;
|
|
|
|
return theta;
|
|
}
|
|
|
|
double geocentric_latitude(double b)
|
|
{
|
|
return -b;
|
|
}
|
|
|
|
double mean_elongation_moon_sun(double jce)
|
|
{
|
|
return third_order_polynomial(1.0/189474.0, -0.0019142, 445267.11148, 297.85036, jce);
|
|
}
|
|
|
|
double mean_anomaly_sun(double jce)
|
|
{
|
|
return third_order_polynomial(-1.0/300000.0, -0.0001603, 35999.05034, 357.52772, jce);
|
|
}
|
|
|
|
double mean_anomaly_moon(double jce)
|
|
{
|
|
return third_order_polynomial(1.0/56250.0, 0.0086972, 477198.867398, 134.96298, jce);
|
|
}
|
|
|
|
double argument_latitude_moon(double jce)
|
|
{
|
|
return third_order_polynomial(1.0/327270.0, -0.0036825, 483202.017538, 93.27191, jce);
|
|
}
|
|
|
|
double ascending_longitude_moon(double jce)
|
|
{
|
|
return third_order_polynomial(1.0/450000.0, 0.0020708, -1934.136261, 125.04452, jce);
|
|
}
|
|
|
|
double xy_term_summation(int i, double x[TERM_X_COUNT])
|
|
{
|
|
int j;
|
|
double sum=0;
|
|
|
|
for (j = 0; j < TERM_Y_COUNT; j++)
|
|
sum += x[j]*Y_TERMS[i][j];
|
|
|
|
return sum;
|
|
}
|
|
|
|
void nutation_longitude_and_obliquity(double jce, double x[TERM_X_COUNT], double *del_psi,
|
|
double *del_epsilon)
|
|
{
|
|
int i;
|
|
double xy_term_sum, sum_psi=0, sum_epsilon=0;
|
|
|
|
for (i = 0; i < Y_COUNT; i++) {
|
|
xy_term_sum = deg2rad(xy_term_summation(i, x));
|
|
sum_psi += (PE_TERMS[i][TERM_PSI_A] + jce*PE_TERMS[i][TERM_PSI_B])*sin(xy_term_sum);
|
|
sum_epsilon += (PE_TERMS[i][TERM_EPS_C] + jce*PE_TERMS[i][TERM_EPS_D])*cos(xy_term_sum);
|
|
}
|
|
|
|
*del_psi = sum_psi / 36000000.0;
|
|
*del_epsilon = sum_epsilon / 36000000.0;
|
|
}
|
|
|
|
double ecliptic_mean_obliquity(double jme)
|
|
{
|
|
double u = jme/10.0;
|
|
|
|
return 84381.448 + u*(-4680.93 + u*(-1.55 + u*(1999.25 + u*(-51.38 + u*(-249.67 +
|
|
u*( -39.05 + u*( 7.12 + u*( 27.87 + u*( 5.79 + u*2.45)))))))));
|
|
}
|
|
|
|
double ecliptic_true_obliquity(double delta_epsilon, double epsilon0)
|
|
{
|
|
return delta_epsilon + epsilon0/3600.0;
|
|
}
|
|
|
|
double aberration_correction(double r)
|
|
{
|
|
return -20.4898 / (3600.0*r);
|
|
}
|
|
|
|
double apparent_sun_longitude(double theta, double delta_psi, double delta_tau)
|
|
{
|
|
return theta + delta_psi + delta_tau;
|
|
}
|
|
|
|
double greenwich_mean_sidereal_time (double jd, double jc)
|
|
{
|
|
return limit_degrees(280.46061837 + 360.98564736629 * (jd - 2451545.0) +
|
|
jc*jc*(0.000387933 - jc/38710000.0));
|
|
}
|
|
|
|
double greenwich_sidereal_time (double nu0, double delta_psi, double epsilon)
|
|
{
|
|
return nu0 + delta_psi*cos(deg2rad(epsilon));
|
|
}
|
|
|
|
double geocentric_right_ascension(double lamda, double epsilon, double beta)
|
|
{
|
|
double lamda_rad = deg2rad(lamda);
|
|
double epsilon_rad = deg2rad(epsilon);
|
|
|
|
return limit_degrees(rad2deg(atan2(sin(lamda_rad)*cos(epsilon_rad) -
|
|
tan(deg2rad(beta))*sin(epsilon_rad), cos(lamda_rad))));
|
|
}
|
|
|
|
double geocentric_declination(double beta, double epsilon, double lamda)
|
|
{
|
|
double beta_rad = deg2rad(beta);
|
|
double epsilon_rad = deg2rad(epsilon);
|
|
|
|
return rad2deg(asin(sin(beta_rad)*cos(epsilon_rad) +
|
|
cos(beta_rad)*sin(epsilon_rad)*sin(deg2rad(lamda))));
|
|
}
|
|
|
|
double observer_hour_angle(double nu, double longitude, double alpha_deg)
|
|
{
|
|
return limit_degrees(nu + longitude - alpha_deg);
|
|
}
|
|
|
|
double sun_equatorial_horizontal_parallax(double r)
|
|
{
|
|
return 8.794 / (3600.0 * r);
|
|
}
|
|
|
|
void right_ascension_parallax_and_topocentric_dec(double latitude, double elevation,
|
|
double xi, double h, double delta, double *delta_alpha, double *delta_prime)
|
|
{
|
|
double delta_alpha_rad;
|
|
double lat_rad = deg2rad(latitude);
|
|
double xi_rad = deg2rad(xi);
|
|
double h_rad = deg2rad(h);
|
|
double delta_rad = deg2rad(delta);
|
|
double u = atan(0.99664719 * tan(lat_rad));
|
|
double y = 0.99664719 * sin(u) + elevation*sin(lat_rad)/6378140.0;
|
|
double x = cos(u) + elevation*cos(lat_rad)/6378140.0;
|
|
|
|
delta_alpha_rad = atan2( - x*sin(xi_rad) *sin(h_rad),
|
|
cos(delta_rad) - x*sin(xi_rad) *cos(h_rad));
|
|
|
|
*delta_prime = rad2deg(atan2((sin(delta_rad) - y*sin(xi_rad))*cos(delta_alpha_rad),
|
|
cos(delta_rad) - x*sin(xi_rad) *cos(h_rad)));
|
|
|
|
*delta_alpha = rad2deg(delta_alpha_rad);
|
|
}
|
|
|
|
double topocentric_right_ascension(double alpha_deg, double delta_alpha)
|
|
{
|
|
return alpha_deg + delta_alpha;
|
|
}
|
|
|
|
double topocentric_local_hour_angle(double h, double delta_alpha)
|
|
{
|
|
return h - delta_alpha;
|
|
}
|
|
|
|
double topocentric_elevation_angle(double latitude, double delta_prime, double h_prime)
|
|
{
|
|
double lat_rad = deg2rad(latitude);
|
|
double delta_prime_rad = deg2rad(delta_prime);
|
|
|
|
return rad2deg(asin(sin(lat_rad)*sin(delta_prime_rad) +
|
|
cos(lat_rad)*cos(delta_prime_rad) * cos(deg2rad(h_prime))));
|
|
}
|
|
|
|
double atmospheric_refraction_correction(double pressure, double temperature,
|
|
double atmos_refract, double e0)
|
|
{
|
|
double del_e = 0;
|
|
|
|
if (e0 >= -1*(SUN_RADIUS + atmos_refract))
|
|
del_e = (pressure / 1010.0) * (283.0 / (273.0 + temperature)) *
|
|
1.02 / (60.0 * tan(deg2rad(e0 + 10.3/(e0 + 5.11))));
|
|
|
|
return del_e;
|
|
}
|
|
|
|
double topocentric_elevation_angle_corrected(double e0, double delta_e)
|
|
{
|
|
return e0 + delta_e;
|
|
}
|
|
|
|
double topocentric_zenith_angle(double e)
|
|
{
|
|
return 90.0 - e;
|
|
}
|
|
|
|
double topocentric_azimuth_angle_astro(double h_prime, double latitude, double delta_prime)
|
|
{
|
|
double h_prime_rad = deg2rad(h_prime);
|
|
double lat_rad = deg2rad(latitude);
|
|
|
|
return limit_degrees(rad2deg(atan2(sin(h_prime_rad),
|
|
cos(h_prime_rad)*sin(lat_rad) - tan(deg2rad(delta_prime))*cos(lat_rad))));
|
|
}
|
|
|
|
double topocentric_azimuth_angle(double azimuth_astro)
|
|
{
|
|
return limit_degrees(azimuth_astro + 180.0);
|
|
}
|
|
|
|
double surface_incidence_angle(double zenith, double azimuth_astro, double azm_rotation,
|
|
double slope)
|
|
{
|
|
double zenith_rad = deg2rad(zenith);
|
|
double slope_rad = deg2rad(slope);
|
|
|
|
return rad2deg(acos(cos(zenith_rad)*cos(slope_rad) +
|
|
sin(slope_rad )*sin(zenith_rad) * cos(deg2rad(azimuth_astro - azm_rotation))));
|
|
}
|
|
|
|
double sun_mean_longitude(double jme)
|
|
{
|
|
return limit_degrees(280.4664567 + jme*(360007.6982779 + jme*(0.03032028 +
|
|
jme*(1/49931.0 + jme*(-1/15300.0 + jme*(-1/2000000.0))))));
|
|
}
|
|
|
|
double eot(double m, double alpha, double del_psi, double epsilon)
|
|
{
|
|
return limit_minutes(4.0*(m - 0.0057183 - alpha + del_psi*cos(deg2rad(epsilon))));
|
|
}
|
|
|
|
double approx_sun_transit_time(double alpha_zero, double longitude, double nu)
|
|
{
|
|
return (alpha_zero - longitude - nu) / 360.0;
|
|
}
|
|
|
|
double sun_hour_angle_at_rise_set(double latitude, double delta_zero, double h0_prime)
|
|
{
|
|
double h0 = -99999;
|
|
double latitude_rad = deg2rad(latitude);
|
|
double delta_zero_rad = deg2rad(delta_zero);
|
|
double argument = (sin(deg2rad(h0_prime)) - sin(latitude_rad)*sin(delta_zero_rad)) /
|
|
(cos(latitude_rad)*cos(delta_zero_rad));
|
|
|
|
if (fabs(argument) <= 1) h0 = limit_degrees180(rad2deg(acos(argument)));
|
|
|
|
return h0;
|
|
}
|
|
|
|
void approx_sun_rise_and_set(double *m_rts, double h0)
|
|
{
|
|
double h0_dfrac = h0/360.0;
|
|
|
|
m_rts[SUN_RISE] = limit_zero2one(m_rts[SUN_TRANSIT] - h0_dfrac);
|
|
m_rts[SUN_SET] = limit_zero2one(m_rts[SUN_TRANSIT] + h0_dfrac);
|
|
m_rts[SUN_TRANSIT] = limit_zero2one(m_rts[SUN_TRANSIT]);
|
|
}
|
|
|
|
double rts_alpha_delta_prime(double *ad, double n)
|
|
{
|
|
double a = ad[JD_ZERO] - ad[JD_MINUS];
|
|
double b = ad[JD_PLUS] - ad[JD_ZERO];
|
|
|
|
if (fabs(a) >= 2.0) a = limit_zero2one(a);
|
|
if (fabs(b) >= 2.0) b = limit_zero2one(b);
|
|
|
|
return ad[JD_ZERO] + n * (a + b + (b-a)*n)/2.0;
|
|
}
|
|
|
|
double rts_sun_altitude(double latitude, double delta_prime, double h_prime)
|
|
{
|
|
double latitude_rad = deg2rad(latitude);
|
|
double delta_prime_rad = deg2rad(delta_prime);
|
|
|
|
return rad2deg(asin(sin(latitude_rad)*sin(delta_prime_rad) +
|
|
cos(latitude_rad)*cos(delta_prime_rad)*cos(deg2rad(h_prime))));
|
|
}
|
|
|
|
double sun_rise_and_set(double *m_rts, double *h_rts, double *delta_prime, double latitude,
|
|
double *h_prime, double h0_prime, int sun)
|
|
{
|
|
return m_rts[sun] + (h_rts[sun] - h0_prime) /
|
|
(360.0*cos(deg2rad(delta_prime[sun]))*cos(deg2rad(latitude))*sin(deg2rad(h_prime[sun])));
|
|
}
|
|
|
|
////////////////////////////////////////////////////////////////////////////////////////////////
|
|
// Calculate required SPA parameters to get the right ascension (alpha) and declination (delta)
|
|
// Note: JD must be already calculated and in structure
|
|
////////////////////////////////////////////////////////////////////////////////////////////////
|
|
void calculate_geocentric_sun_right_ascension_and_declination(spa_data *spa)
|
|
{
|
|
double x[TERM_X_COUNT];
|
|
|
|
spa->jc = julian_century(spa->jd);
|
|
|
|
spa->jde = julian_ephemeris_day(spa->jd, spa->delta_t);
|
|
spa->jce = julian_ephemeris_century(spa->jde);
|
|
spa->jme = julian_ephemeris_millennium(spa->jce);
|
|
|
|
spa->l = earth_heliocentric_longitude(spa->jme);
|
|
spa->b = earth_heliocentric_latitude(spa->jme);
|
|
spa->r = earth_radius_vector(spa->jme);
|
|
|
|
spa->theta = geocentric_longitude(spa->l);
|
|
spa->beta = geocentric_latitude(spa->b);
|
|
|
|
x[TERM_X0] = spa->x0 = mean_elongation_moon_sun(spa->jce);
|
|
x[TERM_X1] = spa->x1 = mean_anomaly_sun(spa->jce);
|
|
x[TERM_X2] = spa->x2 = mean_anomaly_moon(spa->jce);
|
|
x[TERM_X3] = spa->x3 = argument_latitude_moon(spa->jce);
|
|
x[TERM_X4] = spa->x4 = ascending_longitude_moon(spa->jce);
|
|
|
|
nutation_longitude_and_obliquity(spa->jce, x, &(spa->del_psi), &(spa->del_epsilon));
|
|
|
|
spa->epsilon0 = ecliptic_mean_obliquity(spa->jme);
|
|
spa->epsilon = ecliptic_true_obliquity(spa->del_epsilon, spa->epsilon0);
|
|
|
|
spa->del_tau = aberration_correction(spa->r);
|
|
spa->lamda = apparent_sun_longitude(spa->theta, spa->del_psi, spa->del_tau);
|
|
spa->nu0 = greenwich_mean_sidereal_time (spa->jd, spa->jc);
|
|
spa->nu = greenwich_sidereal_time (spa->nu0, spa->del_psi, spa->epsilon);
|
|
|
|
spa->alpha = geocentric_right_ascension(spa->lamda, spa->epsilon, spa->beta);
|
|
spa->delta = geocentric_declination(spa->beta, spa->epsilon, spa->lamda);
|
|
}
|
|
|
|
////////////////////////////////////////////////////////////////////////
|
|
// Calculate Equation of Time (EOT) and Sun Rise, Transit, & Set (RTS)
|
|
////////////////////////////////////////////////////////////////////////
|
|
|
|
void calculate_eot_and_sun_rise_transit_set(spa_data *spa)
|
|
{
|
|
spa_data sun_rts;
|
|
double nu, m, h0, n;
|
|
double alpha[JD_COUNT], delta[JD_COUNT];
|
|
double m_rts[SUN_COUNT], nu_rts[SUN_COUNT], h_rts[SUN_COUNT];
|
|
double alpha_prime[SUN_COUNT], delta_prime[SUN_COUNT], h_prime[SUN_COUNT];
|
|
double h0_prime = -1*(SUN_RADIUS + spa->atmos_refract);
|
|
int i;
|
|
|
|
sun_rts = *spa;
|
|
m = sun_mean_longitude(spa->jme);
|
|
spa->eot = eot(m, spa->alpha, spa->del_psi, spa->epsilon);
|
|
|
|
sun_rts.hour = sun_rts.minute = sun_rts.second = 0;
|
|
sun_rts.delta_ut1 = sun_rts.timezone = 0.0;
|
|
|
|
sun_rts.jd = julian_day (sun_rts.year, sun_rts.month, sun_rts.day, sun_rts.hour,
|
|
sun_rts.minute, sun_rts.second, sun_rts.delta_ut1, sun_rts.timezone);
|
|
|
|
calculate_geocentric_sun_right_ascension_and_declination(&sun_rts);
|
|
nu = sun_rts.nu;
|
|
|
|
sun_rts.delta_t = 0;
|
|
sun_rts.jd--;
|
|
for (i = 0; i < JD_COUNT; i++) {
|
|
calculate_geocentric_sun_right_ascension_and_declination(&sun_rts);
|
|
alpha[i] = sun_rts.alpha;
|
|
delta[i] = sun_rts.delta;
|
|
sun_rts.jd++;
|
|
}
|
|
|
|
m_rts[SUN_TRANSIT] = approx_sun_transit_time(alpha[JD_ZERO], spa->longitude, nu);
|
|
h0 = sun_hour_angle_at_rise_set(spa->latitude, delta[JD_ZERO], h0_prime);
|
|
|
|
if (h0 >= 0) {
|
|
|
|
approx_sun_rise_and_set(m_rts, h0);
|
|
|
|
for (i = 0; i < SUN_COUNT; i++) {
|
|
|
|
nu_rts[i] = nu + 360.985647*m_rts[i];
|
|
|
|
n = m_rts[i] + spa->delta_t/86400.0;
|
|
alpha_prime[i] = rts_alpha_delta_prime(alpha, n);
|
|
delta_prime[i] = rts_alpha_delta_prime(delta, n);
|
|
|
|
h_prime[i] = limit_degrees180pm(nu_rts[i] + spa->longitude - alpha_prime[i]);
|
|
|
|
h_rts[i] = rts_sun_altitude(spa->latitude, delta_prime[i], h_prime[i]);
|
|
}
|
|
|
|
spa->srha = h_prime[SUN_RISE];
|
|
spa->ssha = h_prime[SUN_SET];
|
|
spa->sta = h_rts[SUN_TRANSIT];
|
|
|
|
spa->suntransit = dayfrac_to_local_hr(m_rts[SUN_TRANSIT] - h_prime[SUN_TRANSIT] / 360.0,
|
|
spa->timezone);
|
|
|
|
spa->sunrise = dayfrac_to_local_hr(sun_rise_and_set(m_rts, h_rts, delta_prime,
|
|
spa->latitude, h_prime, h0_prime, SUN_RISE), spa->timezone);
|
|
|
|
spa->sunset = dayfrac_to_local_hr(sun_rise_and_set(m_rts, h_rts, delta_prime,
|
|
spa->latitude, h_prime, h0_prime, SUN_SET), spa->timezone);
|
|
|
|
} else spa->srha= spa->ssha= spa->sta= spa->suntransit= spa->sunrise= spa->sunset= -99999;
|
|
|
|
}
|
|
|
|
///////////////////////////////////////////////////////////////////////////////////////////
|
|
// Calculate all SPA parameters and put into structure
|
|
// Note: All inputs values (listed in header file) must already be in structure
|
|
///////////////////////////////////////////////////////////////////////////////////////////
|
|
int spa_calculate(spa_data *spa)
|
|
{
|
|
int result;
|
|
|
|
result = validate_inputs(spa);
|
|
|
|
if (result == 0)
|
|
{
|
|
spa->jd = julian_day (spa->year, spa->month, spa->day, spa->hour,
|
|
spa->minute, spa->second, spa->delta_ut1, spa->timezone);
|
|
|
|
calculate_geocentric_sun_right_ascension_and_declination(spa);
|
|
|
|
spa->h = observer_hour_angle(spa->nu, spa->longitude, spa->alpha);
|
|
spa->xi = sun_equatorial_horizontal_parallax(spa->r);
|
|
|
|
right_ascension_parallax_and_topocentric_dec(spa->latitude, spa->elevation, spa->xi,
|
|
spa->h, spa->delta, &(spa->del_alpha), &(spa->delta_prime));
|
|
|
|
spa->alpha_prime = topocentric_right_ascension(spa->alpha, spa->del_alpha);
|
|
spa->h_prime = topocentric_local_hour_angle(spa->h, spa->del_alpha);
|
|
|
|
spa->e0 = topocentric_elevation_angle(spa->latitude, spa->delta_prime, spa->h_prime);
|
|
spa->del_e = atmospheric_refraction_correction(spa->pressure, spa->temperature,
|
|
spa->atmos_refract, spa->e0);
|
|
spa->e = topocentric_elevation_angle_corrected(spa->e0, spa->del_e);
|
|
|
|
spa->zenith = topocentric_zenith_angle(spa->e);
|
|
spa->azimuth_astro = topocentric_azimuth_angle_astro(spa->h_prime, spa->latitude,
|
|
spa->delta_prime);
|
|
spa->azimuth = topocentric_azimuth_angle(spa->azimuth_astro);
|
|
|
|
if ((spa->function == SPA_ZA_INC) || (spa->function == SPA_ALL))
|
|
spa->incidence = surface_incidence_angle(spa->zenith, spa->azimuth_astro,
|
|
spa->azm_rotation, spa->slope);
|
|
|
|
if ((spa->function == SPA_ZA_RTS) || (spa->function == SPA_ALL))
|
|
calculate_eot_and_sun_rise_transit_set(spa);
|
|
}
|
|
|
|
return result;
|
|
}
|
|
///////////////////////////////////////////////////////////////////////////////////////////
|