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 millisecond timing precision mode. Millisecond timing precision mode is deprecated and will be removed in a future release. We recommend that you migrate your Mission Plans to nanosecond timing precision mode.

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

Method Signature

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

Arguments

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

Return Value

Type:

number

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

Syntax

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