Struct EquinoctialElements

Namespace

NominalSystems.Universe

Assembly

NominalSystems.Universe.dll

[Nominal] This structure contains the set of Equinoctial elements that define the spacecraft translational state.

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public struct EquinoctialElements

Constructors

EquinoctialElements()

Default constructor

public EquinoctialElements()

EquinoctialElements(double, double, double, double, double, double, double)

Constructs a new equinoctial elements with all of the correct values

public EquinoctialElements(double semiMajorAxis, double p1, double p2, double q1, double q2, double l, double ll)

Parameters

semiMajorAxis double

[m] The Semi-Major Axis of the Body

p1 double

[-] e*sin(omega+Omega)

p2 double

[-] e*cos(omega+Omega)

q1 double

[-] tan(i/2)*sin(Omega)

q2 double

[-] tan(i/2)*cos(Omega)

l double

[-] Omega+omega+M

ll double

[-] Omega+omega+f

Fields

L

[-] Omega+omega+M

public double L

Field Value

double

LL

[-] Omega+omega+f

public double LL

Field Value

double

P1

[-] e*sin(omega+Omega)

public double P1

Field Value

double

P2

[-] e*cos(omega+Omega)

public double P2

Field Value

double

Q1

[-] tan(i/2)*sin(Omega)

public double Q1

Field Value

double

Q2

[-] tan(i/2)*cos(Omega)

public double Q2

Field Value

double

SemiMajorAxis

[m] The Semi-Major Axis of the Body

public double SemiMajorAxis

Field Value

double