Roll Attitude Control for Flying Wing via Apex Vortex Perturbation
Year: 2026
Type: article
Source: AIAA Journal
DOI: 10.2514/1.j066379
Authors: Qi-Ming Wang, Li-Hao Feng
Institution: Beihang University
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Award: G8198715552
OpenAlex ID: W7128050626
