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196 lines
6.1 KiB
C
196 lines
6.1 KiB
C
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//
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// Plan13.cpp
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//
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// An implementation of Plan13 in C++ by Mark VandeWettering
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//
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// Plan13 is an algorithm for satellite orbit prediction first formulated
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// by James Miller G3RUH. I learned about it when I saw it was the basis
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// of the PIC based antenna rotator project designed by G6LVB.
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//
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// http://www.g6lvb.com/Articles/LVBTracker2/index.htm
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//
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// I ported the algorithm to Python, and it was my primary means of orbit
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// prediction for a couple of years while I operated the "Easy Sats" with
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// a dual band hand held and an Arrow antenna.
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//
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// I've long wanted to redo the work in C++ so that I could port the code
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// to smaller processors including the Atmel AVR chips. Bruce Robertson,
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// VE9QRP started the qrpTracker project to fufill many of the same goals,
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// but I thought that the code could be made more compact and more modular,
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// and could serve not just the embedded targets but could be of more
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// use for more general applications. And, I like the BSD License a bit
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// better too.
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//
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// So, here it is!
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//
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/*
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Copyright 2011, Mark VandeWettering. All rights reserved.
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Redistribution and use in source and binary forms, with or without
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modification, are permitted provided that the following conditions are
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met:
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1. Redistributions of source code must retain the above copyright
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notice, this list of conditions and the following disclaimer.
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2. Redistributions in binary form must reproduce the above copyright
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notice, this list of conditions and the following disclaimer
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in the documentation and/or other materials provided with the
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distribution.
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THIS SOFTWARE IS PROVIDED BY MARK VANDEWETTERING ''AS IS'' AND ANY
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EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT LIMITED TO, THE
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IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS FOR A PARTICULAR
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PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL <COPYRIGHT HOLDER> OR
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CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, INCIDENTAL, SPECIAL,
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EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, BUT NOT LIMITED TO,
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PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS OF USE, DATA, OR
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PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED AND ON ANY THEORY OF
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LIABILITY, WHETHER IN CONTRACT, STRICT LIABILITY, OR TORT (INCLUDING
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NEGLIGENCE OR OTHERWISE) ARISING IN ANY WAY OUT OF THE USE OF THIS
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SOFTWARE, EVEN IF ADVISED OF THE POSSIBILITY OF SUCH DAMAGE.
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The views and conclusions contained in the software and documentation
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are those of the authors and should not be interpreted as representing
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official policies, either expressed or implied, of Mark VandeWettering
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*/
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// Modification by Anthony Good, K3NG 2020-07-24: Change DateTime to SatDateTime to avoid a conflict with an RTC library I'm using
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//----------------------------------------------------------------------
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#if defined(ARDUINO) && ARDUINO >= 100
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#include "Arduino.h"
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#else
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#include "WProgram.h"
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#endif
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// here are a bunch of constants that will be used throughout the
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// code, but which will probably not be helpful outside.
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static const double RE = 6378.137f ;
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static const double FL = 1.f/298.257224f ;
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static const double GM = 3.986E5f ;
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static const double J2 = 1.08263E-3f ;
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static const double YM = 365.25f ;
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static const double YT = 365.2421874f ;
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static const double WW = 2.f*M_PI/YT ;
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static const double WE = 2.f*M_PI+ WW ;
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static const double W0 = WE/86400.f ;
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static const double YG = 2014.f;
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static const double G0 = 99.5828f;
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static const double MAS0 = 356.4105f;
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static const double MASD = 0.98560028f;
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static const double EQC1 = 0.03340;
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static const double EQC2 = 0.00035;
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static const double INS = radians(23.4375f);
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// static const double YG = 2000.f ;
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// static const double G0 = 98.9821f ;
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// static const double MAS0 = 356.0507f ;
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// static const double MASD = 0.98560028f ;
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// static const double EQC1 = 0.03342 ;
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// static const double EQC2 = 0.00035 ;
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// static const double INS = radians(23.4393f) ;
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static const double CNS = cos(INS) ;
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static const double SNS = sin(INS) ;
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//----------------------------------------------------------------------
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// the original BASIC code used three variables (e.g. Ox, Oy, Oz) to
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// represent a vector quantity. I think that makes for slightly more
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// obtuse code, so I going to collapse them into a single variable
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// which is an array of three elements
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typedef double Vec3[3] ;
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//----------------------------------------------------------------------
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class SatDateTime {
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public:
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long DN ;
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double TN ;
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SatDateTime(int year, int month, int day, int h, int m, int s) ;
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SatDateTime(const SatDateTime &) ;
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SatDateTime() ;
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~SatDateTime() { }
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void add(double) ;
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void settime(int year, int month, int day, int h, int m, int s) ;
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void gettime(int& year, int& mon, int& day, int& h, int& m, int& s) ;
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void ascii(char *) ;
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void roundup(double) ;
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} ;
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//----------------------------------------------------------------------
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class Observer {
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public:
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const char *name ;
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double LA ;
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double LO ;
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double HT ;
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Vec3 U, E, N, O, V ;
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Observer(const char *, double, double, double) ;
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~Observer() { } ;
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} ;
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//----------------------------------------------------------------------
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class Satellite {
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long N ;
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long YE ;
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long DE ;
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double TE ;
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double IN ;
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double RA ;
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double EC ;
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double WP ;
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double MA ;
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double MM ;
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double M2 ;
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double RV ;
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double ALON ;
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double ALAT ;
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// these values are stored, but could be calculated on the fly
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// during calls to predict()
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// classic space/time tradeoff
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double N0, A_0, B_0 ;
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double PC ;
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double QD, WD, DC ;
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double RS ;
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public:
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const char *name ;
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Vec3 SAT, VEL ; // celestial coordinates
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Vec3 S, V ; // geocentric coordinates
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Satellite() { } ;
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Satellite(const char *name, const char *l1, const char *l2) ;
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~Satellite() ;
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void tle(const char *name, const char *l1, const char *l2) ;
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void predict(const SatDateTime &dt) ;
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void LL(double &lat, double &lng) ;
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void altaz(const Observer &obs, double &alt, double &az) ;
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} ;
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class Sun {
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public:
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Vec3 SUN, H ;
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Sun() ;
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~Sun() { } ;
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void predict(const SatDateTime &dt) ;
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void LL(double &lat, double &lng) ;
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void altaz(const Observer &obs, double &alt, double &az) ;
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} ;
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