UAM Landing
Landing Approach Surfaces Performance, Constraint, and Accuracy Analysis
- Landing approach surfaces design and performance analysis in terms of energy, power, and time
- Constraint analysis considering inflow modeling, vortex ring state (VRS), acceleration limits, h-V (dead man’s) diagram, speed limits, obstacles, and FAA regulations
- Landing simulations under turbulence using retrofitted tilt-wing flight dynamic models and landing accuracy analysis via circular error probables