Orbit.hpp

// orbit.h
//
// Copyright (C) 2001, Chris Laurel <claurel@shatters.net>
//
// CometOrbit: Copyright (C) 2007,2008 Johannes Gajdosik
//             Amendments (c) 2013 Georg Zotti
//
// This program is free software; you can redistribute it and/or
// modify it under the terms of the GNU General Public License
// as published by the Free Software Foundation; either version 2
// of the License, or (at your option) any later version.

#ifndef _ORBIT_HPP_
#define _ORBIT_HPP_

#include "VecMath.hpp"

class OrbitSampleProc;

class Orbit
{
public:
    Orbit(void) {}
    virtual ~Orbit(void) {}
private:
    Orbit(const Orbit&);
    const Orbit &operator=(const Orbit&);
};


class EllipticalOrbit : public Orbit
{
public:
    EllipticalOrbit(double pericenterDistance,
            double eccentricity,
            double inclination,
            double ascendingNode,
            double argOfPeriapsis,
            double meanAnomalyAtEpoch,
            double period,
            double epoch,           // = 2451545.0,
            double parentRotObliquity,  // = 0.0,
            double parentRotAscendingnode,  // = 0.0
            double parentRotJ2000Longitude  // = 0.0
            );

    // Compute position for a specified Julian date and return coordinates
    // given in "dynamical equinox and ecliptic J2000"
    // which is the reference frame for VSOP87
    // In order to rotate to VSOP87
    // parentRotObliquity and parentRotAscendingnode must be supplied.
    void positionAtTimevInVSOP87Coordinates(const double JDE, double* v) const;

    // Original one
    Vec3d positionAtTime(const double JDE) const;
    double getPeriod() const;
    double getBoundingRadius() const;
    virtual void sample(double, double, int, OrbitSampleProc&) const;

private:
    double eccentricAnomaly(const double M) const;
    Vec3d positionAtE(const double E) const;

    double pericenterDistance;
    double eccentricity;
    double inclination;
    double ascendingNode;
    double argOfPeriapsis;
    double meanAnomalyAtEpoch;
    double period;
    double epoch;
    double rotateToVsop87[9];
};


class CometOrbit : public Orbit {
public:
    CometOrbit(double pericenterDistance,
           double eccentricity,
           double inclination,
           double ascendingNode,
           double argOfPerhelion,
           double timeAtPerihelion,
           double orbitGoodDays,
           double meanMotion,           // GZ: for parabolics, this is W/dt in Heafner's lettering
           double parentRotObliquity,       // Comets only have parent==sun, no need for these? Oh yes, VSOP/J2000 eq frames!
           double parentRotAscendingnode,
           double parentRotJ2000Longitude
           );
    // Compute the orbit for a specified Julian day and return a "stellarium compliant" function
    // GZ: new optional variable: updateVelocityVector, true required for dust tail orientation!
    void positionAtTimevInVSOP87Coordinates(double JDE, double* v, bool updateVelocityVector=true);
    // updating the tails is a bit expensive. try not to overdo it.
    bool getUpdateTails() const { return updateTails; }
    void setUpdateTails(const bool update){ updateTails=update; }
    Vec3d getVelocity() const { return rdot; }
    double getSemimajorAxis() const { return (e==1. ? 0. : q / (1.-e)); }
    double getEccentricity() const { return e; }
    bool objectDateValid(const double JDE) const { return (fabs(t0-JDE)<orbitGood); }
private:
    const double q;  
    const double e;  
    const double i;  
    const double Om; 
    const double w;  
    const double t0; 
    const double n;  
    Vec3d rdot;      
    double rotateToVsop87[9]; 
    bool updateTails; 
    const double orbitGood; 
};


class OrbitSampleProc
{
 public:
    virtual ~OrbitSampleProc() {;}
    virtual void sample(const Vec3d&) = 0;
};

/*
 * Stuff found unused and deactivated pre-0.15

// Custom orbit classes should be derived from CachingOrbit.  The custom
// orbits can be expensive to compute, with more than 50 periodic terms.
// Celestia may need require position of a Planet more than once per frame; in
// order to avoid redundant calculation, the CachingOrbit class saves the
// result of the last calculation and uses it if the time matches the cached
// time.
class CachingOrbit : public Orbit
{
public:
    CachingOrbit() : lastTime(1.0e-30) {} //;

    virtual Vec3d computePosition(double JDE) const = 0;
    virtual double getPeriod() const = 0;
    virtual double getBoundingRadius() const = 0;

    Vec3d positionAtTime(double JDE) const;

    virtual void sample(double, double, int, OrbitSampleProc& proc) const;

private:
    mutable Vec3d lastPosition;
    mutable double lastTime;
};

*/

#endif // _ORBIT_HPP_