OrbitFrameECEF Class Reference
[Orbit Frames]

#include <OrbitFrameECEF.h>

Inheritance diagram for OrbitFrameECEF:

[legend]List of all members.

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Detailed Description

Earth-Centered, Earth-Fixed Satellite Coordinate System.

Detailed Description.

Definition at line 21 of file OrbitFrameECEF.h.

Public Member Functions
Rotation	GetRotationFromIJK () const
	Return the rotation ignores transformation due to precession, nutation, and polar motion. .
virtual Rotation	GetRotation2IJK () const=0
virtual OrbitFrame *	NewPointer ()=0
virtual OrbitFrame *	Clone ()=0
Public Attributes
OrbitFrameECEF(const double &_ApparentSiderealTime) Rotatio	GetRotation2IJK )() const
	Constructor Return the rotation ignores transformation due to precession, nutation, and polar motion. .

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Member Function Documentation

Rotation OrbitFrameECEF::GetRotationFromIJK (   )  const [virtual]

Return the rotation ignores transformation due to precession, nutation, and polar motion. . Parameters: _ApparentSiderealTime  Apparent Sidereal Time (rad) Returns: rotation from IJK to ECEF Implements OrbitFrame. Definition at line 43 of file OrbitFrameECEF.h.

virtual Rotation OrbitFrame::GetRotation2IJK (   )  const [pure virtual, inherited]

Implemented in OrbitFrameIJK, OrbitFrameNTW, OrbitFramePQW, and OrbitFrameSEZ.

virtual OrbitFrame* OrbitFrame::NewPointer (   )  [pure virtual, inherited]

Implemented in OrbitFrameIJK, OrbitFrameNTW, OrbitFramePQW, and OrbitFrameRSW.

virtual OrbitFrame* OrbitFrame::Clone (   )  [pure virtual, inherited]

Implemented in OrbitFrameIJK, OrbitFrameNTW, OrbitFramePQW, and OrbitFrameRSW.

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Member Data Documentation

OrbitFrameECEF (const double &_ApparentSiderealTime) Rotatio OrbitFrameECEF::GetRotation2IJK)() const

Constructor Return the rotation ignores transformation due to precession, nutation, and polar motion. . Parameters: _ApparentSiderealTime  Apparent Sidereal Time (rad) Returns: rotation from ECEF to IJK Definition at line 35 of file OrbitFrameECEF.h.

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