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java.lang.Objectkeps.PropagationModel
keps.SGP0
public class SGP0
This class implements the SGP0 Orbital Propagation model.
| Constructor Summary | |
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SGP0()
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| Method Summary | |
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void |
update(Satellite sat,
double tsince,
Vector3 pos,
Vector3 velo)
The abstract update method implements the propagation model which, provided a satellite and a time, calculates a position and velocity for the object. |
| Methods inherited from class java.lang.Object |
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equals, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait |
| Constructor Detail |
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public SGP0()
| Method Detail |
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public void update(Satellite sat,
double tsince,
Vector3 pos,
Vector3 velo)
update in class PropagationModelsat - Satellite The satellite to be propagated.tsince - double The time at which predictions should be made.pos - Vector3 The ECI position vector populated by the model.velo - Vector3 The ECI velocity vector populated by the model.
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