OrbitState Struct Reference

Inheritance diagram for OrbitState:

Collaboration diagram for OrbitState:

Public Member Functions
OrbitState &	operator+= (double rhs)
OrbitState &	operator*= (double rhs)
OrbitState	operator+ (double rhs) const
OrbitState	operator+ (const OrbitState &rhs) const
OrbitState	operator* (double rhs) const
Public Member Functions inherited from OrbitOptions
OrbitOptions &	operator+= (const OrbitOptions &rhs)

Data Fields
SatSys	Sat
string	str
bool	exclude = false
shared_ptr< KFState >	subState_ptr
vector< EMP >	empInput
map< E_Component, double >	componentsMap
int	numEmp = 0
int	numParam = 0
double	srpCr = 0
double	dragCd = 0
Vector3d	pos
Vector3d	vel
MatrixXd	posVelSTM
bool	estimateCr = false
bool	estimateCd = false
AttStatus	attStatus
Vector3d	gyroBias = Vector3d::Zero()
Vector3d	acclBias = Vector3d::Zero()
Vector3d	gyroScale = Vector3d::Ones()
Vector3d	acclScale = Vector3d::Ones()
double	posVar = 0
Data Fields inherited from OrbitOptions
double	mass = 1000
double	area = 20
double	power = 20
double	srp_cr = 1.25
double	drag_cd = 2.2
vector< E_ThirdBody >	planetary_perturbations
bool	empirical = true
bool	antenna_thrust = true
E_SRPModel	albedo = E_SRPModel::NONE
E_SRPModel	solar_radiation_pressure = E_SRPModel::NONE
bool	drag = false
vector< bool >	empirical_dyb_eclipse = {true}
vector< bool >	empirical_rtn_eclipse = {false}
vector< SurfaceDetails >	surface_details
struct {
bool   enable = false
int   interval = 0
vector< double >   epochs = {}
double   pos_proc_noise = 10
double   vel_proc_noise = 5
}	pseudoPulses
map< int, bool >	initialisedMap

Member Function Documentation

operator*()

OrbitState OrbitState::operator* ( double rhs ) const

inline

operator*=()

OrbitState & OrbitState::operator*= ( double rhs )

inline

operator+() [1/2]

OrbitState OrbitState::operator+ ( const OrbitState & rhs ) const

inline

operator+() [2/2]

OrbitState OrbitState::operator+ ( double rhs ) const

inline

operator+=()

OrbitState & OrbitState::operator+= ( double rhs )

inline

Field Documentation

acclBias

Vector3d OrbitState::acclBias = Vector3d::Zero()

acclScale

Vector3d OrbitState::acclScale = Vector3d::Ones()

attStatus

AttStatus OrbitState::attStatus

componentsMap

map<E_Component, double> OrbitState::componentsMap

mutable

dragCd

double OrbitState::dragCd = 0

empInput

vector<EMP> OrbitState::empInput

estimateCd

bool OrbitState::estimateCd = false

estimateCr

bool OrbitState::estimateCr = false

exclude

bool OrbitState::exclude = false

gyroBias

Vector3d OrbitState::gyroBias = Vector3d::Zero()

gyroScale

Vector3d OrbitState::gyroScale = Vector3d::Ones()

numEmp

int OrbitState::numEmp = 0

numParam

int OrbitState::numParam = 0

pos

Vector3d OrbitState::pos

posVar

double OrbitState::posVar = 0

posVelSTM

MatrixXd OrbitState::posVelSTM

Sat

SatSys OrbitState::Sat

srpCr

double OrbitState::srpCr = 0

str

string OrbitState::str

subState_ptr

shared_ptr<KFState> OrbitState::subState_ptr

vel

Vector3d OrbitState::vel

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The documentation for this struct was generated from the following file:

• /ginan/src/cpp/orbprop/orbitProp.hpp