Estimation with ParameterDriver

Orekit usage
1

Hello,

I am trying to do orbit determination using the KalmanEstimator provided by Orekit. My objective is to estimate the orbit (the 6 orbital parameters) but also the drag coefficient of my satellite.
To do so, I select the parameterDriver “drag coefficient” of my numercialPropagatorBuilder as “true”. Then, I create my KalmanEstimatorBuilder using this numericalPropagatorBuilder. Finaly, I get the value of the drag coefficient after each estimation step.

// Drag force
double dragCoef = 1000.; //the dragCoeff used to generate the measures is equal to 2.2
IsotropicDrag dragModel = new IsotropicDrag(crossSectionMass, dragCoef);
DragForce dragForce = new DragForce(constants.atmosphere, dragModel);
numericalPropagatorBuilder.addForceModel(dragForce);
    	
// Parameter driver
ParameterDriver dragDriver = numericalPropagatorBuilder.getPropagationParametersDrivers().findByName("drag coefficient");
dragDriver.setSelected(true);

and :

for(ObservedMeasurement<?> measure : measurementsSetsList.get(0)) {
  Propagator[] propagatorEstimated = kalmanEstimator.estimationStep(measure);
  ParameterDriversList propagatorParameters = kalmanEstimator.getPropagationParametersDrivers(true);
  List<ParameterDriver> list = new ArrayList<>(propagatorParameters.getDrivers());
  for(ParameterDriver driver : list) {
    if (driver.getName().equals("drag coefficient")) {
      System.out.println(driver.getValue());
    }
}

However, it seems that the value of the drag coefficient is not estimated by the filter, as its value doesn’t change at all from its initial value, even when I set it with an aberrant value.

I suppose I made a mistake using the ParameterDriver class but I really don’t see where…

Thanks in advance for your help!

Paul

2

Hi @paul2

Welcome to the Orekit forum!

It’s just a test, could you try:

                DragForce dragForce = new DragForce(constants.atmosphere, dragModel);
                for (final ParameterDriver driver : dragForce.getParametersDrivers()) {
                    if (driver.getName().equals(DragSensitive.DRAG_COEFFICIENT)) {
                        driver.setSelected(true);
                    }
                }
               numericalPropagatorBuilder.addForceModel(dragForce);

Regards,
Bryan

3

Thank you for your quick answer!
I tried to use your code but it didn’t change, the value of the drag coefficient is always equal to its initial value.
Regards,
paul

4

Hi @paul2,

What is your initial orbit ?

Could you send us a runnable test case ?

Thanks,
Maxime

5

Hi,
For my initial orbit, I am using the ISS orbit :

    	double i = 51.6416*Math.PI/180;
    	double raan = 247.4627*Math.PI/180;
    	double e = 0.0006703;
    	double pa = 130.5360*Math.PI/180;
    	double anomaly = 61.6196828895407;
    	double rev_day = 15.72125391;
    	double T = 3600*24/rev_day;
    	double a = Math.cbrt(Math.pow(T, 2)*mu/(4*Math.pow(Math.PI,2)));

Please find a runnable case :
test_OD.java (9.6 KB)

Regards,
Paul