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//
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// cEci.h
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//
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// Copyright (c) 2003 Michael F. Henry
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//
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#pragma once
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#include "cVector.h"
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#include "cJulian.h"
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#include "coord.h"
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//////////////////////////////////////////////////////////////////////
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// class cEci
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// Encapsulates an Earth-Centered Inertial position, velocity, and time.
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class cEci
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{
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public:
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cEci() { m_VecUnits = UNITS_NONE; }
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cEci(const cCoordGeo &geo, const cJulian &cJulian);
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cEci(const cVector &pos, const cVector &vel,
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const cJulian &date, bool IsAeUnits = true);
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virtual ~cEci() {};
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cCoordGeo toGeo();
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cVector getPos() const { return m_pos; }
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cVector getVel() const { return m_vel; }
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cJulian getDate() const { return m_date; }
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void setUnitsAe() { m_VecUnits = UNITS_AE; }
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void setUnitsKm() { m_VecUnits = UNITS_KM; }
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bool UnitsAreAe() const { return m_VecUnits == UNITS_AE; }
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bool UnitsAreKm() const { return m_VecUnits == UNITS_KM; }
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void ae2km(); // Convert position, velocity vector units from AE to km
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protected:
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void MulPos(double factor) { m_pos.Mul(factor); }
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void MulVel(double factor) { m_vel.Mul(factor); }
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enum VecUnits
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{
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UNITS_NONE, // not initialized
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UNITS_AE,
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UNITS_KM,
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};
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cVector m_pos;
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cVector m_vel;
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cJulian m_date;
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VecUnits m_VecUnits;
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};
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