EADS Innovation Works, as research center of EADS, has been involved recently in the development of inverse methods for trajectory tools.
Two aerospace applications will be presented with a focus on inverse problem and first automatic differentiation (AD) experiments using the Tapenade tool, developed at INRIA Sophia-Antipolis TROPICS team.
- Identification of the aerodynamics coefficients of a probe for different flight conditions (Mach number, angle of attack), given trajectories measurements : the final objective is to obtain a reliable prediction of dynamic stability of this probe, using an adapted numerical trajectory scheme (Runge Kutta) and large scale coefficients parameterization.
- Identification of heat flux coefficient from time domain temperature measurements. The industrial objective is the thermal protection system dimensioning problem for atmospheric re-entry missions of aerospace vehicles. The problem is applied on a transient one-dimensional thermal model with one moving boundary (ablative surface), with degradable thermal materials.
For these two applications, the inverse problem is also formulated as a minimization problem with optimal control formulation (lagrangian, adjoint and gradients computations, with optimization loop). To compute numerically the adjoint and gradient quantities, we have used both analytical differentiation and Automatic Differentiation. First encouraging results of automatic differentiation procedure on these industrial applications will be presented, with validations in agreement with measurements.