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- W642854986 abstract "A parallel hybrid dynamic programming approach for trajectory optimization is proposed. The application of this approach is exemplified by ascent trajectory optimization for an aerospace plane. The proposed algorithm is based on the combined utilization with the forward dynamic programming and the branch-and-bound method, and makes possible to obtain routinely and robustly numerical solutions to achieve the minimum-fuel ascent to Low-Earth-Orbit under complicated constraints. The lower bound of cost function required in this algorithm implementation is calculated by the energy-state approximation which is very effective in producing considerable reductions in computation requirements of the hybrid algorithm as well as storage requirements. An application to the preliminary design of aerospace planes are included." @default.
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- W642854986 date "1997-06-01" @default.
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- W642854986 title "Parallel Hybrid Dynamic Programming Approach to Aerospace Plane Performance Optimization" @default.
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- W642854986 doi "https://doi.org/10.1016/s1474-6670(17)43847-x" @default.
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