TY - JOUR
T1 - Hierarchical Optimization Algorithm and Applications of Spacecraft Trajectory Optimization
AU - He, Hanqing
AU - Shi, Peng
AU - Zhao, Yushan
N1 - Publisher Copyright:
© 2022 by the authors. Li-censee MDPI, Basel, Switzerland.
PY - 2022/2
Y1 - 2022/2
N2 - The pursuit of excellent performance in meta-heuristic algorithms has led to a myriad of extensive and profound research and achievements. Notably, many space mission planning problems are solved with the help of meta-heuristic algorithms, and relevant studies continue to appear. This paper introduces a hierarchical optimization frame in which two types of particles—B-particles and S-particles—synergistically search for the optima. Global exploration relies on B-particles, whose motional direction and step length are designed independently. S-particles are for fine local exploitation near the current best B-particle. Two specific algorithms are designed according to this frame. New variants of classical benchmark functions are used to better test the proposed algo-rithms. Furthermore, two spacecraft trajectory optimization problems, spacecraft multi-impulse orbit transfer and the pursuit-evasion game of two spacecraft, are employed to examine the applica-bility of the proposed algorithms. The simulation results indicate that the hierarchical optimization algorithms perform well on given trials and have great potential for space mission planning.
AB - The pursuit of excellent performance in meta-heuristic algorithms has led to a myriad of extensive and profound research and achievements. Notably, many space mission planning problems are solved with the help of meta-heuristic algorithms, and relevant studies continue to appear. This paper introduces a hierarchical optimization frame in which two types of particles—B-particles and S-particles—synergistically search for the optima. Global exploration relies on B-particles, whose motional direction and step length are designed independently. S-particles are for fine local exploitation near the current best B-particle. Two specific algorithms are designed according to this frame. New variants of classical benchmark functions are used to better test the proposed algo-rithms. Furthermore, two spacecraft trajectory optimization problems, spacecraft multi-impulse orbit transfer and the pursuit-evasion game of two spacecraft, are employed to examine the applica-bility of the proposed algorithms. The simulation results indicate that the hierarchical optimization algorithms perform well on given trials and have great potential for space mission planning.
KW - Hierarchical optimization algorithm
KW - Meta-heuristics
KW - Multi-impulse orbit transfer
KW - Spacecraft pursuit-evasion game
UR - https://www.scopus.com/pages/publications/85124294913
U2 - 10.3390/aerospace9020081
DO - 10.3390/aerospace9020081
M3 - 文章
AN - SCOPUS:85124294913
SN - 2226-4310
VL - 9
JO - Aerospace
JF - Aerospace
IS - 2
M1 - 81
ER -