Description
Returns whether the specified look ahead
propagator is supported
Syntax
| [Visual Basic .NET] |
|---|
Public Function IsLookAheadPropagatorSupported( _
ByVal Propagator As AgELookAheadPropagator _
) As Boolean
|
| [C#] |
|---|
public bool IsLookAheadPropagatorSupported(
|
| [Managed C++] |
|---|
public: bool IsLookAheadPropagatorSupported(
|
| [Java] |
|---|
public bool isLookAheadPropagatorSupported(
|
| [Unmanaged C++] |
|---|
public: HRESULT IsLookAheadPropagatorSupported(
|
Parameters
- Propagator
-
Member Value Description eLookAheadUnknown -1 Reserved for look ahead propagators that are not currently supported eLookAheadHoldCBIPosition 0 The HoldCBIPosition look ahead propagator keeps position and velocity constant in the inertial (i.e., CBI) frame. eLookAheadHoldCBFPosition 1 The HoldCBFPosition look ahead propagator keeps position and velocity constant in the fixed (i.e., CBF) frame. eLookAheadTwoBody 2 Two-Body is an analytical propagator that generates ephemeris by evaluating a formula. eLookAheadJ2Perturbation 3 The J2 Perturbation (first-order) propagator accounts for secular variations in the orbit elements due to Earth oblateness. eLookAheadJ4Perturbation 4 The J4 Perturbation (second-order) propagator accounts for secular variations in the orbit elements due to Earth oblateness. eLookAheadDeadReckon 5 The DeadReckon look ahead propagator projects the motion of the vehicle along a straight line, along the last velocity vector. eLookAheadBallistic 6 The Ballistic Propagator defines an elliptical path that begins and ends at the Earth's surface. Specifying a fixed flight time, initial velocity or altitude can further refine the shape of the trajectory.