@inproceedings{95692af9f62e49e9824d8c2dd6164af2,
title = "Reachable-Orbit-Domain for Launch Vehicles Based on Polyhedron Approximation Method",
abstract = "This paper focuses on the onboard generation of reachable-orbit-domain for launch vehicles. We solve a series of optimal control problem to generate the max-volume inscribed polyhedron to approximate the reachable domain for the launch vehicle, by using convex optimization algorithm.",
keywords = "Optimal Control, Reachable-oribit-domian, Second-Order Cone Programming",
author = "Zeming Hao and Haifeng Hu and Yong He and Huifeng Li",
note = "Publisher Copyright: {\textcopyright} 2022 ACA.; 13th Asian Control Conference, ASCC 2022 ; Conference date: 04-05-2022 Through 07-05-2022",
year = "2022",
doi = "10.23919/ASCC56756.2022.9828333",
language = "英语",
series = "ASCC 2022 - 2022 13th Asian Control Conference, Proceedings",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "2447--2449",
booktitle = "ASCC 2022 - 2022 13th Asian Control Conference, Proceedings",
address = "美国",
}