This paper proposes a continuity equation-based debris' evolutionary model for the long-term propagation of fragments' clouds under atmospheric drag, J2 perturbation, solar radiation pressure and third-body perturbation. In particular, it focuses on enhancing the computational efficiency of the dynamical model. This purpose is achieved by cutting off some long-term effects of the perturbations, through averaging of the dynamics equations, and by deriving analytical expressions for the Earth's and Moon's ephemerides, through least squares fitting method. A new cost-free computation of the needed trace of the Jacobian for conservative forces is also proposed. The paper includes a validation phase, where the tool is applied to the modelling and propagation of two fragmentation clouds, characterised by a different dynamical regime, which allows to preliminarily identify some boundaries of applicability of the implemented dynamical model.

Phase Space Description of the Debris’ Cloud Dynamics Through a Continuum Approach

Giudici, L.;Trisolini, M.;Colombo, C.
2022-01-01

Abstract

This paper proposes a continuity equation-based debris' evolutionary model for the long-term propagation of fragments' clouds under atmospheric drag, J2 perturbation, solar radiation pressure and third-body perturbation. In particular, it focuses on enhancing the computational efficiency of the dynamical model. This purpose is achieved by cutting off some long-term effects of the perturbations, through averaging of the dynamics equations, and by deriving analytical expressions for the Earth's and Moon's ephemerides, through least squares fitting method. A new cost-free computation of the needed trace of the Jacobian for conservative forces is also proposed. The paper includes a validation phase, where the tool is applied to the modelling and propagation of two fragmentation clouds, characterised by a different dynamical regime, which allows to preliminarily identify some boundaries of applicability of the implemented dynamical model.
2022
73rd International Astronautical Congress (IAC 2022)
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11311/1223380
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