Abstract
Space domain awareness (SDA) has become increasingly important as industry and society seek further interest in occupying space for surveillance, communication, and environmental services. To maintain safe launch and orbit-placement of future satellites, there is a need to reliably track the positions and trajectories of discarded launch designs that are debris objects orbiting Earth. In particular, debris with sizes on the order of 20 cm or smaller travelling at high speeds maintain enough energy to pierce and permanently damage current, functional satellites. To monitor debris, the Dynamic Data Driven Applications Systems (DDDAS) paradigm can enhance accuracy with object modeling and observational updates. This paper presents a theoretical analysis of modeling the radar returns of space debris as simulated signatures for comparison to real measurements. For radar modeling, when the incident radiation wavelength is comparable to the radius of the debris object, Mie scattering is dominant. Mie scattering describes situations where the radiation scatter propagates predominantly, i.e., contains the greatest power density, along the same direction as the incident wave. Mie scatter modeling is especially useful when tracking objects with forward scatter bistatic radar, as the transmitter, target, and receiver lie along the same geometrical trajectory. The Space Watch Observing Radar Debris Signatures (SWORDS) baseline method involves modeling the radar cross-sections (RCS) of space debris signatures in relation to the velocity and rotational motions of space debris. The results show the impact of the debris radii varying from 20 cm down to 1 cm when illuminated by radiation of comparable wavelength. The resulting scattering nominal mathematical relationships determine how debris size and motion affects the radar signature. The SWORDS method demonstrates that the RCS is proportional to linear size, and that the Doppler shift is predominantly influenced by translation motion.
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Acknowledgments
We thank Dr. Erik Blasch for concept development and paper editing. Partial research support through the Air Force Office of Scientific Research (AFOSR) Grant Number FA9550-20-1-0176 is acknowledged. The views and conclusions contained herein are those of the authors and should not be interpreted as necessarily representing the official policies or endorsements, either expressed or implied, of the Air Force Research Laboratory or the U.S. Government.
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Henry, J.K.A., Narayanan, R.M., Singla, P. (2024). Radar Cross-Section Modeling of Space Debris. In: Blasch, E., Darema, F., Aved, A. (eds) Dynamic Data Driven Applications Systems. DDDAS 2022. Lecture Notes in Computer Science, vol 13984. Springer, Cham. https://doi.org/10.1007/978-3-031-52670-1_8
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