Table 2 Forward kinematics example 1
From: Design and Analysis for a Three-Rotational-DOF Flight Simulator of Fighter-Aircraft
Parameters | 1 | 2 | 3 | 4 | 5 | 6 | 7 | 8 |
|---|---|---|---|---|---|---|---|---|
\('\theta_{1} \;(\text{rad})\) | 1.89417 | ‒ | ‒ | ‒ | ‒ | ‒ | ‒ | ‒ |
\('\theta_{2} \;(\text{rad})\) | 1.89417 | ‒ | ‒ | ‒ | ‒ | ‒ | ‒ | ‒ |
\('\theta_{3} \;(\text{rad)}\) | 1.89417 | ‒ | ‒ | ‒ | ‒ | ‒ | ‒ | ‒ |
\(\lambda \;(\text{rad)}\) | 0.00000 | ‒ | ‒ | ‒ | ‒ | ‒ | ‒ | ‒ |
\(\varepsilon \;(\text{rad})\) | 0.00000 | ‒ | ‒ | ‒ | ‒ | ‒ | ‒ | ‒ |
\(\upsilon \;(\text{rad})\) | 0.00000 | ‒ | ‒ | ‒ | ‒ | ‒ | ‒ | ‒ |
\(\theta^{\prime}_{1} \;(\text{rad)}\) | 1.89417 | 1.89417 | 1.89417 | − 1.89417 | − 1.89417 | − 1.89417 | − 1.89417 | 1.89417 |
\(\theta^{\prime}_{2}\; (\text{rad})\) | 1.89417 | 1.89417 | − 1.89417 | − 1.89417 | − 1.89417 | 1.89417 | 1.89417 | − 1.89417 |
\(\theta^{\prime}_{3} \;(\text{rad})\) | 1.89417 | − 1.89417 | − 1.89417 | − 1.89417 | 1.89417 | 1.89417 | − 1.89417 | 1.89417 |