Aerodynamic Envelope Computation for Safe Landing of the HL-20 Personnel Launch Vehicle Using Hybrid Control
Year: 2005
Type: conference-paper
Authors: I. Kitsios, J. Lygeros
Institution: University of Patras
Language: English
Subfield: Computational Theory and Mathematics
Field: Computer Science
Domain: Physical Sciences
Open Access status: closed
Funder: European Commission
OpenAlex ID: W1908478556
