AdditionalEquations
is removed@Deprecated public class AdditionalEquationsAdapter extends Object implements AdditionalDerivativesProvider
AdditionalEquations
to AdditionalDerivativesProvider
.Constructor and Description |
---|
AdditionalEquationsAdapter(AdditionalEquations equations,
Supplier<SpacecraftState> stateSupplier)
Deprecated.
Simple constructor.
|
Modifier and Type | Method and Description |
---|---|
double[] |
derivatives(SpacecraftState state)
Deprecated.
Compute the derivatives related to the additional state parameters.
|
int |
getDimension()
Deprecated.
Get the dimension of the generated derivative.
|
String |
getName()
Deprecated.
Get the name of the additional derivatives (which will become state once integrated).
|
void |
init(SpacecraftState initialState,
AbsoluteDate target)
Deprecated.
Initialize the generator at the start of propagation.
|
boolean |
yield(SpacecraftState state)
Deprecated.
Check if this provider should yield so another provider has an opportunity to add missing parts.
|
public AdditionalEquationsAdapter(AdditionalEquations equations, Supplier<SpacecraftState> stateSupplier)
equations
- wrapped equationsstateSupplier
- supplier for reference statepublic String getName()
getName
in interface AdditionalDerivativesProvider
public int getDimension()
getDimension
in interface AdditionalDerivativesProvider
public boolean yield(SpacecraftState state)
Decision to yield is often based on an additional state being already available
in the provided state
(but it could theoretically also depend on
an additional state derivative being already available
, or any other criterion). If for example a provider needs the state transition
matrix, it could implement this method as:
public boolean yield(final SpacecraftState state) {
return !state.getAdditionalStates().containsKey("STM");
}
The default implementation returns false
, meaning that derivative data can be
computed
immediately.
yield
in interface AdditionalDerivativesProvider
state
- state to handlepublic void init(SpacecraftState initialState, AbsoluteDate target)
init
in interface AdditionalDerivativesProvider
initialState
- initial state information at the start of propagationtarget
- date of propagationpublic double[] derivatives(SpacecraftState state)
derivatives
in interface AdditionalDerivativesProvider
state
- current state information: date, kinematics, attitude, and
additional states this equations depend on (according to the
yield
method)Copyright © 2002-2022 CS GROUP. All rights reserved.