Table 3 Forward kinematics example 2
From: Design and Analysis for a Three-Rotational-DOF Flight Simulator of Fighter-Aircraft
Parameters | 1 | 2 | 3 | 4 | 5 | 6 | 7 | 8 |
|---|---|---|---|---|---|---|---|---|
\('\theta_{1} \;(\text{rad})\) | 1.74548 | ‒ | ‒ | ‒ | ‒ | ‒ | ‒ | ‒ |
\('\theta_{2} \;(\text{rad})\) | 2.29808 | ‒ | ‒ | ‒ | ‒ | ‒ | ‒ | ‒ |
\('\theta_{3} \;(\text{rad)}\) | 2.05784 | ‒ | ‒ | ‒ | ‒ | ‒ | ‒ | ‒ |
\(\lambda \;(\text{rad)}\) | 0.10000 | ‒ | ‒ | ‒ | ‒ | ‒ | ‒ | ‒ |
\(\varepsilon \;(\text{rad})\) | 0.10000 | ‒ | ‒ | ‒ | ‒ | ‒ | ‒ | ‒ |
\(\upsilon \;(\text{rad})\) | 0.10000 | ‒ | ‒ | ‒ | ‒ | ‒ | ‒ | ‒ |
\(\theta^{\prime}_{1}\; (\text{rad)}\) | 2.24689 | 2.24689 | 2.24689 | − 1.72881 | − 1.72881 | − 1.72881 | − 1.72881 | 2.24689 |
\(\theta^{\prime}_{2} \;(\text{rad})\) | 1.81504 | 1.81504 | − 2.02941 | − 2.02941 | − 2.02941 | 1.81504 | 1.81504 | − 2.02941 |
\(\theta^{\prime}_{3}\; (\text{rad})\) | 2.08712 | − 1.51476 | − 1.51476 | − 1.51476 | 2.08712 | 2.08712 | − 1.51476 | 2.08712 |