Spacecraft.FrozenMAGuess(Variable, Variable, Variable) Method

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Description

Calculates an estimated mean anomaly of a one-burn maneuver that restores frozen orbit conditions.

Timing Precision Mode

This page describes functionality in nanosecond timing precision mode.

Click here to see the documentation for this object in millisecond timing precision mode.

Spacecraft.FrozenMAGuess(	Variable targetArgumentOfPerigee,
	Variable targetEccentricity,
	Variable deltaV)

targetArgumentOfPerigee
Description:	Target Mean Argument of Perigee
Units:	deg
Valid Range:	-360 ≤ targetArgumentOfPerigee ≤ 360

targetEccentricity
Description:	Target Mean Eccentricity

deltaV
Description:	Estimate of the Maneuver Delta-V
Units:	m/s

Type:

number

Returns an estimated mean anomaly of a one-burn maneuver that restores frozen orbit conditions.

myVariable1 = mySpacecraft1.FrozenMAGuess(myVariable2, myVariable3, myVariable4);