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https://gitlab.ibr.cs.tu-bs.de/tschuber/ns-3-leo.git
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107 lines
2 KiB
C++
107 lines
2 KiB
C++
/* -*- Mode:C++; c-file-style:"gnu"; indent-tabs-mode:nil; -*- */
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#ifndef LEO_CIRCULAR_ORBIT_MOBILITY_MODEL_H
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#define LEO_CIRCULAR_ORBIT_MOBILITY_MODEL_H
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#include "ns3/vector.h"
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#include "ns3/object.h"
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#include "ns3/log.h"
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#include "ns3/mobility-model.h"
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#include "ns3/nstime.h"
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#define LEO_EARTH_RAD_M 6371009.0
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#define LEO_EARTH_GM 3.98600436e14
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namespace ns3 {
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/**
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* \ingroup leo
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* \brief Keep track of the orbital postion and velocity of a satellite.
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*
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* This uses simple circular orbits based on the inclination of the orbital
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* plane and the height of the satellite.
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*/
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class LeoCircularOrbitMobilityModel : public MobilityModel
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{
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public:
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/**
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* Register this type with the TypeId system.
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* \return the object TypeId
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*/
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static TypeId GetTypeId (void);
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LeoCircularOrbitMobilityModel ();
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virtual ~LeoCircularOrbitMobilityModel ();
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/**
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* km/s
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*/
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double GetSpeed () const;
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double GetAltitude () const;
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void SetAltitude (double h);
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double GetLatitude () const;
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void SetLatitude (double lat);
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double GetOffset () const;
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void SetOffset (double off);
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double GetInclination () const;
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void SetInclination (double incl);
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private:
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/**
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* Orbit height in m
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*/
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double m_orbitHeight;
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/**
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* Inclination in rad
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*/
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double m_inclination;
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/**
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* Latitude in rad
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*/
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double m_latitude;
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/**
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* Offset on the orbital plane in rad
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*/
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double m_offset;
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/**
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* Normal vector of orbital plane.
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*/
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Vector3D m_plane;
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/**
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* \return the current position.
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*/
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virtual Vector DoGetPosition (void) const;
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/**
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* \param position the position to set.
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*/
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virtual void DoSetPosition (const Vector &position);
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/**
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* \return the current velocity.
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*/
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virtual Vector DoGetVelocity (void) const;
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/**
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* Get the normal vector of the orbital plane
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*/
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Vector3D PlaneNorm () const;
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double GetProgress (Time t) const;
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/**
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* Advances a satellite by a degrees on the orbital plane
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*/
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Vector3D RotatePlane (double a, const Vector3D &x) const;
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};
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}
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#endif
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