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Costate mapping for indirect trajectory optimization
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作者 Ehsan Taheri vishala arya John L.Junkins 《Astrodynamics》 EI CSCD 2021年第4期359-371,共13页
Numerical solutions of optimal control problems are influenced by the appropriate choice of coordinates.The proposed method based on the variational approach to map costates between sets of coordinates and/or elements... Numerical solutions of optimal control problems are influenced by the appropriate choice of coordinates.The proposed method based on the variational approach to map costates between sets of coordinates and/or elements is suitable for solving optimal control problems using the indirect formalism of optimal control theory.The Jacobian of the nonlinear map between any two sets of coordinates and elements is a key component of costate vector mapping theory.A new solution for the class of planar,free-terminal-time,minimum-time,orbit rendezvous maneuvers is also presented.The accuracy of the costate mapping is verified,and its utility is demonstrated by solving minimum-time and minimum-fuel spacecraft trajectory optimization problems. 展开更多
关键词 indirect optimization SPACECRAFT trajectory optimization optimal control theory minimum time minimum fuel INTERPLANETARY Earth-centered low thrust
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