The cyclogyro, as an innovative type of aircraft, has attracted widespread attention owing to its distinctive design and potential in vertical takeoff and landing, low-speed maneuverability, and overall efficiency. However, its intricate aerodynamic traits present challenges in sustaining high flight performance across different conditions. This study systematically explores methods to enhance the flight performance of the cyclogyro using dynamic control strategies. The key focus of the research lies in boosting aerodynamic efficiency, enhancing flight stability, and minimizing the complexity of the control system. Adaptive aerodynamic control techniques are utilized to dynamically adjust the airfoil and actively manage the airflow, effectively delaying flow separation, reducing air resistance, and thereby markedly enhancing lift and flight stability. Furthermore, this study incorporates rational control methods by combining Model Predictive Control with Proportional-Integral-Derivative hybrid strategies to enhance system response speed and robustness. The findings demonstrate that dynamic control strategies are essential for enhancing the aerodynamic efficiency and flight performance of rotorcraft. This study offers valuable insights for advancing cyclogyro engineering and realizing efficient and stable flight across diverse conditions.