yodaUtility/sgp4/cNoradSGP4.h

//
// cNoradSGP4.h
//
// This class implements the NORAD Simple General Perturbation 4 orbit
// model. This model provides the ECI coordiantes/velocity of satellites
// with orbit periods less than 225 minutes.
//
// Copyright (c) 2003 Michael F. Henry
//
#pragma once

#include "cNoradBase.h"

class cOrbit;

//////////////////////////////////////////////////////////////////////////////
class cNoradSGP4 : public cNoradBase
{
public:
   cNoradSGP4(const cOrbit &orbit);
   ~cNoradSGP4(void);

   virtual bool getPosition(double tsince, cEci &eci);

protected:
   double m_c5; 
   double m_omgcof;
   double m_xmcof;
   double m_delmo;
   double m_sinmo;
};
1	//
2	// cNoradSGP4.h
3	//
4	// This class implements the NORAD Simple General Perturbation 4 orbit
5	// model. This model provides the ECI coordiantes/velocity of satellites
6	// with orbit periods less than 225 minutes.
7	//
8	// Copyright (c) 2003 Michael F. Henry
9	//
10	#pragma once
11
12	#include "cNoradBase.h"
13
14	class cOrbit;
15
16	//////////////////////////////////////////////////////////////////////////////
17	class cNoradSGP4 : public cNoradBase
18	{
19	public:
20	cNoradSGP4(const cOrbit &orbit);
21	~cNoradSGP4(void);
22
23	virtual bool getPosition(double tsince, cEci &eci);
24
25	protected:
26	double m_c5;
27	double m_omgcof;
28	double m_xmcof;
29	double m_delmo;
30	double m_sinmo;
31	};