Figure 6
From: Visual augmentation of deck-landing-ability improves helicopter ship landing decisions
Distributions of touchdown velocity resulting from attempting deck-landing (\({V}_{td}^{attempt}\)) and predicted when aborting deck-landing (\({V}_{td}^{abort}\)) for Control (A, B) and Augmentation conditions (C, D) and for LL (A–C) and HL (B–D) groups. The red dotted vertical line depicts \({V}_{crt}\) and separates the safe touchdown velocities from unsafe ones.
