From: Design and Analysis for a Three-Rotational-DOF Flight Simulator of Fighter-Aircraft
\(\theta^{\prime}_{1} (\text{rad)}\) | \(\theta^{\prime}_{2} (rad)\) | \(\theta^{\prime}_{3} (rad)\) | \(\lambda \;(\text{rad)}\) | \(\varepsilon \;(rad)\) | \(\upsilon \;(rad)\) | \(\varphi \;\left( {rad} \right)\) | \(\lambda^{\prime}\;(rad)\) | \(\varepsilon^{\prime}\;(rad)\) | \(\upsilon^{\prime}\;(rad)\) |
---|---|---|---|---|---|---|---|---|---|
1.74548 | 2.29808 | 2.05784 | 0.10000 | 0.10000 | 0.10000 | 3π/5 | − 0.12601 | 0.06420 | 0.10000 |