SpacecraftParam.hpp

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#pragma once
 
#include "AstGlobal.h"
 
AST_NAMESPACE_BEGIN
 
class AST_CORE_API SpacecraftParam
{
public:
    SpacecraftParam() = default;
    ~SpacecraftParam() = default;
public:
    double cd() const { return cd_; }
    void setCd(double cd) { cd_ = cd; }
 
    double cr() const { return cr_; }
    void setCr(double cr) { cr_ = cr; }
 
    double dragArea() const { return dragArea_; }
    void setDragArea(double dragArea) { dragArea_ = dragArea; }
    
    double srpArea() const { return srpArea_; }
    void setSrpArea(double srpArea) { srpArea_ = srpArea; }
 
    double mass() const { return dryMass_ + fuelMass_; }
 
    double dryMass() const { return dryMass_; }
    void setDryMass(double dryMass) { dryMass_ = dryMass; }
 
    double fuelMass() const { return fuelMass_; }
    void setFuelMass(double fuelMass) { fuelMass_ = fuelMass; }
 
    double fuelDensity() const { return fuelDensity_; }
    void setFuelDensity(double fuelDensity) { fuelDensity_ = fuelDensity; }
 
    double k1() const { return k1_; }
    void setK1(double k1) { k1_ = k1; }
    
    double k2() const { return k2_; }
    void setK2(double k2) { k2_ = k2; }
 
    double radPressureArea() const { return radPressureArea_; }
    void setRadPressureArea(double radPressureArea) { radPressureArea_ = radPressureArea; }
    
    double radPressureCoeff() const { return radPressureCoeff_; }
    void setRadPressureCoeff(double radPressureCoeff) { radPressureCoeff_ = radPressureCoeff; }
 
    double tankPressure() const { return tankPressure_; }
    void setTankPressure(double tankPressure) { tankPressure_ = tankPressure; }
 
    double tankTemperature() const { return tankTemperature_; }
    void setTankTemperature(double tankTemperature) { tankTemperature_ = tankTemperature; }
protected:
    double cd_{2.2};                         
    double cr_{1};                           
    double dragArea_{20};                    
    double srpArea_{20};                     
    double dryMass_{500};                    
    double fuelMass_{500};                   
    double fuelDensity_{1000};               
    double k1_{1};                           
    double k2_{1};                           
    double radPressureArea_{20};             
    double radPressureCoeff_{1};             
    double tankPressure_{5000};              
    double tankTemperature_{293.15};         
};
 
AST_NAMESPACE_END