DEIMOS
Earth Observation Mission CFI Software
Orbit Software User Manual
for JAVA
ESA

PropagModelEnum

Propagation models. More...

Variables

static long EECFI::EnumOrbit.XOCFI_PROPAG_MODEL_MEAN_KEPL = 0
 Propagation using Mean Keplerian OSV model.
static long EECFI::EnumOrbit.XOCFI_PROPAG_MODEL_SPOT = 1
 Propagation using Spot model.
static long EECFI::EnumOrbit.XOCFI_PROPAG_MODEL_TLE = 2
 Propagation using TLE model.
static long EECFI::EnumOrbit.XOCFI_PROPAG_MODEL_PRECISE = 3
 Propagation using COWELL propagator.
static long EECFI::EnumOrbit.XOCFI_PROPAG_MODEL_AUTO = 10
 Propagation using Auto initialization model.
static long EECFI::EnumOrbit.XOCFI_PROPAG_MODEL_DOUBLE = 100
 Propagation using double initialization model.

Detailed Description

Propagation models.


Variable Documentation

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

Propagation using Auto initialization model.

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

Propagation using double initialization model.

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

Propagation using Mean Keplerian OSV model.

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

Propagation using COWELL propagator.

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

Propagation using Spot model.

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

Propagation using TLE model.


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