Processing of altimetric data for precise orbit determination

The challenging science objectives of future planetary missions will require highly accurate trajectory reconstruction of deep space probes. Novel techniques to improve the navigation capabilities are being developed with the purpose to expand the scientific return of geophysical investigations across the Solar System. Science instruments that provide geodetic data from the spacecraft orbit may support the orbit determination process in combination with deep space radio tracking measurements. Altimetric data, for example, measure the relative distance of the spacecraft with respect to the celestial body's surface, yielding key constraints on the orbit evolution. Observations that are repeated over the same location (i.e., crossover) are less prone to errors associated with surface mismodeling, leading to significant improvements in the estimation of the spacecraft position. In this work, we present a method based on the combination of ground-based radio science and altimetric crossover measurements to enhance the estimation of the spacecraft orbit and geodetic parameters. The software is developed to carry out thorough numerical simulations of mission scenarios, including the generation of synthetic observables. We show the results of our covariance analysis by simulating and processing gravimetric and altimetric measurements that will be collected by future planetary missions.