PropagModelEnum

Propagation models. More...

Variables
static final long	EECFI::EnumOrbit.XOCFI_PROPAG_MODEL_NOT_INITIALIZED = -1
	Propagator not initialized.
static final long	EECFI::EnumOrbit.XOCFI_PROPAG_MODEL_MEAN_KEPL = 0
	Propagation using Mean Keplerian OSV model.
static final long	EECFI::EnumOrbit.XOCFI_PROPAG_MODEL_SPOT = 1
	Propagation using Spot model.
static final long	EECFI::EnumOrbit.XOCFI_PROPAG_MODEL_TLE = 2
	Propagation using TLE model.
static final long	EECFI::EnumOrbit.XOCFI_PROPAG_MODEL_PRECISE = 3
	Propagation using COWELL propagator.
static final long	EECFI::EnumOrbit.XOCFI_PROPAG_MODEL_GEO = 4
	Propagation for geostationary satellites (ANR-353).
static final long	EECFI::EnumOrbit.XOCFI_PROPAG_MODEL_AUTO = 10
	Propagation using Auto initialization model.
static final long	EECFI::EnumOrbit.XOCFI_PROPAG_MODEL_DOUBLE = 100
	Propagation using double initialization model.

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Detailed Description

Propagation models.

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Variable Documentation

final long EECFI.EnumOrbit.XOCFI_PROPAG_MODEL_AUTO = 10 [static, inherited]

Propagation using Auto initialization model.

final long EECFI.EnumOrbit.XOCFI_PROPAG_MODEL_DOUBLE = 100 [static, inherited]

Propagation using double initialization model.

final long EECFI.EnumOrbit.XOCFI_PROPAG_MODEL_GEO = 4 [static, inherited]

Propagation for geostationary satellites (ANR-353).

final long EECFI.EnumOrbit.XOCFI_PROPAG_MODEL_MEAN_KEPL = 0 [static, inherited]

Propagation using Mean Keplerian OSV model.

final long EECFI.EnumOrbit.XOCFI_PROPAG_MODEL_NOT_INITIALIZED = -1 [static, inherited]

Propagator not initialized.

final long EECFI.EnumOrbit.XOCFI_PROPAG_MODEL_PRECISE = 3 [static, inherited]

Propagation using COWELL propagator.

final long EECFI.EnumOrbit.XOCFI_PROPAG_MODEL_SPOT = 1 [static, inherited]

Propagation using Spot model.

final long EECFI.EnumOrbit.XOCFI_PROPAG_MODEL_TLE = 2 [static, inherited]

Propagation using TLE model.