66a7f2ac4c305806813ace5697ef20c674737fbb,src/main/java/org/orekit/propagation/numerical/PartialDerivativesEquations.java,PartialDerivativesEquations,computeDerivatives,#SpacecraftState#number[]#,372
Before Change
// mass corresponds either to a constant or to one free parameter
final DerivativeStructure dsM = (dAccdM == null) ?
new DerivativeStructure(nbVars, 1, s.getMass()) :
new DerivativeStructure(nbVars, 1, 6, s.getMass());
// we should compute attitude partial derivatives with respect to position/velocity
After Change
// mass corresponds either to a constant or to one free parameter
final DerivativeStructure dsM = (dAccdM == null) ?
factory.constant(s.getMass()) :
factory.variable(6, s.getMass());
// we should compute attitude partial derivatives with respect to position/velocity