Zeming Hao, Haifeng Hu 0012, Yong He, Huifeng Li. Reachable-Orbit-Domain for Launch Vehicles Based on Polyhedron Approximation Method. In 13th Asian Control Conference, ASCC 2022, Jeju, Korea, May 4-7, 2022. pages 2447-2449, IEEE, 2022. [doi]
Abstract is missing.