"Reachable-Orbit-Domain for Launch Vehicles Based on Polyhedron ..."

Zeming Hao et al. (2022)

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DOI: 10.23919/ASCC56756.2022.9828333

access: closed

type: Conference or Workshop Paper

metadata version: 2022-08-01

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Zeming Hao, Haifeng Hu, Yong He, Huifeng Li:
Reachable-Orbit-Domain for Launch Vehicles Based on Polyhedron Approximation Method. ASCC 2022: 2447-2449

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