Mapping of the propagation parameters for multi-satellite orbit determination
While performing multi-satellite orbit determination, if a user selects different propagation parameters for each satellite (for example each satellite's SRP coefficient), bugs appear in the class estimation/leastsquares/Model
- An exception occurs in method "createPropagators" as the initial array is too long for each builder;
- The computation of the Jacobian for propagation drivers is wrong in method "fetchEvaluatedMeasurement" as the indexes can be incorrectly mapped in the matrix.
Proposed bug fixes:
- Map each propagator builder's selected propagation drivers so the initial array is correctly sized;
- Map the propagation parameters' columns in the Jacobian in the same fashion as it is done already for measurements parameters.
(from redmine: issue id 354, created on 2017-08-22, closed on 2017-11-25)