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"Reachable-Orbit-Domain for Launch Vehicles Based on Polyhedron ..."
Zeming Hao et al. (2022)
- 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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