Updated UML diagrams with last changes.

src/design/dsst-partial-derivatives-class-diagram.puml

@@ -55,8 +55,8 @@
       	package forces #CCCCC7 {
 
         	interface DSSTForceModel {
-          	   +void initialize()
-        	   +DerivativeStructure[] getMeanElementRate()
+          	   +void init(SpacecraftState initialState, AbsoluteDate target)
+        	   +Gradient[] getMeanElementRate()
                +void updateShortPeriodTerms()
         	}
 
@@ -71,13 +71,15 @@
        }
 
        class DSSTPartialDerivativesEquations {
-          +List<String> getAvailableParameters()
-          +void selectParameters(String ... parameters)
-          +void selectParamAndStep(String parameter, double hP)
-          +void setInitialJacobians()
+          +void freezeParametersSelection()
+          +void setInitialJacobians(SpacecraftState s0)
+          +DSSTJacobiansMapper getMapper()
        }
 
-       class DSSTJacobiansMapper
+       class DSSTJacobiansMapper {
+          +void getStateJacobian(SpacecraftState state, double[][] dYdY0)
+          +void getParametersJacobian(SpacecraftState state, double[][] dYdP)
+       }
 
        AdditionalEquations         <|..     DSSTPartialDerivativesEquations
        DSSTPartialDerivativesEquations *-->     DSSTForceModel

src/design/dsst-propagator-class-diagram.puml

@@ -54,7 +54,7 @@
       class AuxiliaryElements
 
       interface DSSTForceModel {
-        +void initialize(AuxiliaryElements auxiliary, PropagationType type, double[] parameters)
+        +void initializeShortPeriodTerms(AuxiliaryElements auxiliary, PropagationType type, double[] parameters)
         +double[] getMeanElementRate(SpacecraftState state, AuxiliaryElements auxiliary, double[] parameters)
         +void updateShortPeriodTerms(double[] parameters, SpacecraftState ... meanStates)
         +EventDetector[] getEventsDetectors()

src/design/events-class-diagram.puml

@@ -40,7 +40,7 @@
       package handlers #CBDBC8 {
 
         interface "EventHandler<T extends EventDetector>" as EventHandler_T_ {
-          +init(SpacecraftState s0, AbsoluteDate target)
+          +init(SpacecraftState s0, AbsoluteDate target, T detector)
           +Action eventOccurred(SpacecraftState s, T detector, boolean increasing)
           +SpacecraftState resetState(T detector, SpacecraftState oldState)
         }

src/design/generic-ephemeris-writing-class-diagram.puml

@@ -43,15 +43,17 @@
     package files #DDEBD8 {
 
        package sp3 #CBDBC8 {
-          class SP3File
+          class SP3
           class SP3Coordinate
-          SP3File --> SP3Coordinate
+          SP3 --> SP3Coordinate
        }
 
        package ilrs #CBDBC8 {
-         class CPFFile
+         class CPF
+         class CPFWriter
+         class StreamingCpfWriter
          class CPFCoordinate
-         CPFFile --> CPFCoordinate
+         CPF --> CPFCoordinate
        }
 
       package general #CBDBC8 {
@@ -92,8 +94,10 @@
           +getPropagator()
         }
 
-        SP3File ..|> EphemerisFile
-        CPFFile ..|> EphemerisFile
+        SP3 ..|> EphemerisFile
+        CPF ..|> EphemerisFile
+        CPFWriter <--o StreamingCpfWriter
+        EphemerisFileWriter <|.. CPFWriter
         EphemerisFile.SatelliteEphemeris <--* EphemerisFile
         EphemerisFile.SatelliteEphemeris o--> EphemerisFile.EphemerisSegment
 

src/design/kalman-overview-class-diagram.puml

@@ -54,7 +54,7 @@
 
       package sequential #CBDBC8 {
 
-        interface ProcessNoiseMatrixProvider
+        interface CovarianceMatrixProvider
 
         class KalmanEstimator {
           +getOrbitalParametersDrivers()
@@ -64,29 +64,35 @@
           +estimationStep(measurement)
         }
 
-        class Model {
-          +estimationStep(measurement)
+        abstract AbstractKalmanModel {
+          #updateReferenceTrajectories(propagators, pType, sType)
+          #analyticalDerivativeComputations(mapper, state)
+          +ProcessEstimate getEstimate()
+          +EstimatedMeasurement<?> getCorrectedMeasurement()
+          +SpacecraftState[] getCorrectedSpacecraftStates()
         }
 
-        Model <-left-* KalmanEstimator
+        class KalmanModel
+        class DSSTKalmanModel
+        class TLEKalmanModel
+
+        AbstractKalmanModel <-left-* KalmanEstimator
         KalmanEstimator *-right-> ExtendedKalmanFilter_T
-        Model *--> ProcessNoiseMatrixProvider
-        EstimatedMeasurement <-- Model
+        AbstractKalmanModel *--> CovarianceMatrixProvider
+        EstimatedMeasurement <-- AbstractKalmanModel
+        KalmanModel     --|> AbstractKalmanModel
+        DSSTKalmanModel --|> AbstractKalmanModel
+        TLEKalmanModel  --|> AbstractKalmanModel
 
       }
 
     }
 
-    package propagation #DDEBD8 {
-      interface Propagator
-      Propagator <-- Model : run
-    }
-
   }
 
   package user.application #F3EDF7 {
     class MyProcessNoiseMatrixProvider #EAE6F7/B9B3D2
-    ProcessNoiseMatrixProvider <|-- MyProcessNoiseMatrixProvider
+    CovarianceMatrixProvider <|-- MyProcessNoiseMatrixProvider
   }
 
 @enduml

src/design/orbit-determination-measurements-class-diagram.puml

@@ -46,11 +46,11 @@
     
       class EstimatedMeasurement {
         +getObservedMeasurement()
+        +getStateSize()
         +getIteration()
-        +getState()
+        +getStates()
         +getTimeOffset()
-        +[get|set]Value()
-        +[get|set]CurrentWeight()
+        +[get|set]EstimatedValue()
         +[get|set]StateDerivatives()
         +[get|set]ParameterDerivatives()
       }
@@ -59,7 +59,7 @@
         +getParametersDrivers()
         +modify(estimated)
       }
-    
+
       class "On-board antenna" as Onboard
       ObservedMeasurement *--> "*" EstimationModifier
       ObservedMeasurement --> EstimatedMeasurement : create

src/design/partial-derivatives-class-diagram.puml

@@ -33,7 +33,7 @@
 
       interface ForceModel {
         +void addContribution()
-        +FieldVector3D<DerivativeStructure> accelerationDerivatives()
+        +FieldVector3D<Gradient> acceleration()
         +EventDetector[] getEventsDetectors()
       }
 
@@ -68,8 +68,7 @@
 
         interface TimeDerivativesEquations {
           +void addKeplerContribution()
-          +void addXYZAcceleration()
-          +void addAcceleration()
+          +void addNonKeplerianAcceleration()
           +void addMassDerivative()
         }
 
@@ -78,10 +77,9 @@
        }
 
         class PartialDerivativesEquations {
-          +List<String> getAvailableParameters()
-          +void selectParameters(String ... parameters)
-          +void selectParamAndStep(String parameter, double hP)
-          +void setInitialJacobians()
+          +void freezeParametersSelection()
+          +void setInitialJacobians(SpacecraftState s0)
+          +JacobiansMapper getMapper()
        }
       class Jacobianizer
 

src/design/propagator-conversion-class-diagram.puml

@@ -53,6 +53,7 @@
         +setMass(mass)
       }
 
+      class DSSTPropagatorBuilder
       class KeplerianPropagatorBuilder
       class TLEPropagatorBuilder
       class EcksteinHechlerPropagatorBuilder
@@ -85,6 +86,7 @@
       PropagatorBuilder <|.. NumericalPropagatorBuilder
       PropagatorBuilder <|.. KeplerianPropagatorBuilder
       PropagatorBuilder <|.. TLEPropagatorBuilder
+      PropagatorBuilder <|.. DSSTPropagatorBuilder
       PropagatorBuilder <|.right. EcksteinHechlerPropagatorBuilder
 
       PropagatorConverter <|.. AbstractPropagatorConverter