Dynamical mapping of the LEO region for passive disposal design
- Paper number
IAC-17,A6,2,7,x38929
- Author
Dr. Elisa Maria Alessi, IFAC-CNR, Italy
- Coauthor
Dr. Giulia Schettino, IFAC-CNR, Italy
- Coauthor
Dr. Alessandro Rossi, IFAC-CNR, Italy
- Coauthor
Dr. Giovanni Valsecchi, INAF-IAPS, Italy
- Year
2017
- Abstract
We present the results obtained within the H2020 ReDSHIFT project on the dynamical characterization of the Low Earth Orbit (LEO) region. An extended simulation campaign has been performed in order to recognize the dynamical highways that can be exploited for the design of passive disposal strategies. The LEO region has been mapped in terms of semi-major axis, eccentricity, and inclination, by propagating for 120 years a dense grid of initial conditions including quasi-circular up to eccentric orbits, with semi-major axes up to 3000 km in altitude, prograde and retrograde inclinations, 16 combinations of longitude of ascending node and argument of pericenter. For each set of initial conditions, two initial epochs and two values of area-to-mass ratio were considered. The outcome reveals the existence of resonant corridors due to either lunisolar perturbations or solar radiation pressure, which can be used in combination with the atmospheric drag to achieve reentry. The study identified also the main frequencies associated with the orbital elements. Their role is catalogued as a function of semi-major axis and inclination, according to the physical perturbation they correspond to. This information can be exploited, in the long-term simulations of the LEO environment, to devise optimal mitigation scenarios, minimizing the $\Delta$V requirements to comply with a given residual lifetime of the spacecraft. This work is funded through the European Commission Horizon 2020, Framework Programme for Research and Innovation (2014-2020), under the ReDSHIFT project (grant agreement n. 687500).
- Abstract document
- Manuscript document
IAC-17,A6,2,7,x38929.pdf (🔒 authorized access only).
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