Control Synthesis for Hypersonic Vehicle Flight Testing with Input–Output-Sampled Nonlinearities
Year: 2025
Type: article
DOI: 10.2514/1.g008331
Institution: University of Minnesota
Language: English
Subfield: Control and Systems Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Awards: G1509273647, G326916097
OpenAlex ID: W4407353904
