TY - GEN
T1 - Spacecraft trajectory planning using spherical expansion and sequential convex programming
AU - Baldini, Francesca
AU - Foust, Rebecca
AU - Bacula, Alexandra
AU - Chilan, Christian M.
AU - Chung, Soon Jo
AU - Bandyopadhyay, Saptarshi
AU - Rahmani, Amir
AU - De La Croix, Jean Pierre
AU - Hadaegh, Fred Y.
N1 - Publisher Copyright:
© 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2016
Y1 - 2016
N2 - In this paper, we develop a novel algorithm for spacecraft trajectory planning in an uncooperative cluttered environment. The Spherical Expansion and Sequential Convex Programming (SE—SCP) algorithm first uses a spherical expansion based sampling algorithm to explore the workspace. Once a path is found from the start position to the goal position, the algorithm generates a locally optimal trajectory within the homotopy class using sequential convex programming. If the number of samples goes to infinity, then the SE—SCP’s trajectory converges to the globally optimal trajectory in the workspace. The SE—SCP algorithm is computationally efficient, therefore it can be used for real-time applications on resource-constrained systems. We also present numerical simulations and comparisons with existing algorithms.
AB - In this paper, we develop a novel algorithm for spacecraft trajectory planning in an uncooperative cluttered environment. The Spherical Expansion and Sequential Convex Programming (SE—SCP) algorithm first uses a spherical expansion based sampling algorithm to explore the workspace. Once a path is found from the start position to the goal position, the algorithm generates a locally optimal trajectory within the homotopy class using sequential convex programming. If the number of samples goes to infinity, then the SE—SCP’s trajectory converges to the globally optimal trajectory in the workspace. The SE—SCP algorithm is computationally efficient, therefore it can be used for real-time applications on resource-constrained systems. We also present numerical simulations and comparisons with existing algorithms.
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M3 - Conference contribution
AN - SCOPUS:84995542965
SN - 9781624104459
T3 - AIAA/AAS Astrodynamics Specialist Conference, 2016
BT - AIAA/AAS Astrodynamics Specialist Conference, 2016
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA/AAS Astrodynamics Specialist Conference, 2016
Y2 - 13 September 2016 through 16 September 2016
ER -