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	kusanagi	1.1	//
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			};