Research Article
A Multibody Model of Tilt-Rotor Aircraft Based on Kane’s Method
| | (m/s) | Model type | (deg) | (deg) | (cm) | (Nm) |
| | 0 | Single-body | 2.6102 | 2.2694 | 0.8925 | — | | Multibody | 2.6159 | 2.2694 | 0.8945 | 4030 |
| | 10 | Single-body | 2.1558 | 1.5679 | 2.0581 | — | | Multibody | 2.1609 | 1.5676 | 2.06 | 3368 |
| | 20 | Single-body | 1.0758 | 0.1024 | 2.8362 | — | | Multibody | 1.0793 | 0.1016 | 2.8376 | 1876 |
| | 30 | Single-body | -0.0267 | -0.9137 | 3.3743 | — | | Multibody | -0.0242 | -0.9147 | 3.3754 | 420 |
| | 40 | Single-body | -0.9632 | -1.3051 | 3.9133 | — | | Multibody | -0.9612 | -1.3064 | 3.914 | -756 |
| | 50 | Single-body | -1.7255 | -1.208 | 4.6349 | — | | Multibody | -1.7242 | -1.2091 | 4.6351 | -1664 |
| | 60 | Single-body | -2.5659 | -0.4407 | 5.6443 | — | | Multibody | -2.5648 | -0.4422 | 5.6441 | -2936 |
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