| Earth Observation Mission CFI Software Orbit Software User Manual for JAVA |

Variables

# 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.