Review Article
A Review of Wind Tunnel Based Virtual Flight Testing Techniques for Evaluation of Flight Control Systems
Figure 20
Illustration of the five available degrees of freedom [108].
(a) Roll |
(b) Pitch |
(c) Yaw |
(d) Heave |
(e) Sway |
(a) Roll |
(b) Pitch |
(c) Yaw |
(d) Heave |
(e) Sway |