Optimizing blended-wing-body aircraft wing half-spans via reachable sets of linear longitudinal dynamics yields up to 30% lower angle-of-attack tracking error on the resulting nonlinear model under reference tracking control.
Control of Motorcycle Steering Instabilities
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Reachability-Based Design Optimization for Aircraft Maneuverability
Optimizing blended-wing-body aircraft wing half-spans via reachable sets of linear longitudinal dynamics yields up to 30% lower angle-of-attack tracking error on the resulting nonlinear model under reference tracking control.