TY - JOUR
T1 - Analysis of collision avoidance via ground-based laser momentum transfer
AU - Bamann, C.
AU - Hugentobler, U.
AU - Scharring, S.
AU - Kästel, J.
AU - Setty, S. J.
N1 - Publisher Copyright:
© 2020 International Association for the Advancement of Space Safety
PY - 2020/9
Y1 - 2020/9
N2 - There is little potential of action in case of conjunctions where neither chaser nor target can be controlled by spacecraft operators. Nevertheless, potential collisions between such objects pose a significant threat to the space environment. In view of that, some recent studies and developments addressed the concept of momentum transfer (MT) from ground-based lasers for orbit modification and, therefore, collision avoidance. However, achievable Δv increments are highly constrained (pass geometry) and uncertain (tracking accuracy, atmospheric turbulence, object properties). Therefore, we present and study a probabilistic model for MT-based collision avoidance. We derive requirements on laser power, MT success rate, and orbit prediction uncertainty as a function of turbulence compensation capability, time to event, conjunction angle, and area-to-mass ratio. Our results demonstrate capabilities and limitations of the method given currently available technology.
AB - There is little potential of action in case of conjunctions where neither chaser nor target can be controlled by spacecraft operators. Nevertheless, potential collisions between such objects pose a significant threat to the space environment. In view of that, some recent studies and developments addressed the concept of momentum transfer (MT) from ground-based lasers for orbit modification and, therefore, collision avoidance. However, achievable Δv increments are highly constrained (pass geometry) and uncertain (tracking accuracy, atmospheric turbulence, object properties). Therefore, we present and study a probabilistic model for MT-based collision avoidance. We derive requirements on laser power, MT success rate, and orbit prediction uncertainty as a function of turbulence compensation capability, time to event, conjunction angle, and area-to-mass ratio. Our results demonstrate capabilities and limitations of the method given currently available technology.
KW - Astrodynamics
KW - Collision avoidance
KW - Laser momentum transfer
KW - Space debris
UR - http://www.scopus.com/inward/record.url?scp=85088151651&partnerID=8YFLogxK
U2 - 10.1016/j.jsse.2020.07.023
DO - 10.1016/j.jsse.2020.07.023
M3 - Article
AN - SCOPUS:85088151651
SN - 2468-8975
VL - 7
SP - 312
EP - 317
JO - Journal of Space Safety Engineering
JF - Journal of Space Safety Engineering
IS - 3
ER -