Aircraft Control System with Sensor-Driven Plasma Actuators

The patent replaces conventional mechanical control surfaces with plasma actuators that generate plasma forces to control aircraft flight. This substitution eliminates the need for heavy mechanical components while maintaining control functionality, directly addressing the weight reduction goal without sacrificing reliability.

The invention changes the fundamental operating parameter from mechanical force to plasma force. By controlling plasma properties (temperature, density, distribution) through electrical energy input, the system achieves lightweight control while maintaining the ability to generate sufficient aerodynamic forces for stable flight.

The patent replaces the mechanical actuation system with an electromagnetic plasma generation system. Plasma actuators can be rapidly switched on and off and adjusted in real-time without the inertial limitations of mechanical systems, enabling much faster response rates to handle high-frequency disturbances during supersonic and hypersonic flight.

The invention introduces dynamic control through plasma generation that can be rapidly adjusted in real-time. The plasma actuators can be modulated at high frequencies to dynamically counteract disturbances, providing adaptive control that responds much faster than conventional mechanical surfaces.

The patent replaces heavy mechanical control surfaces with lightweight plasma actuators that generate control forces through plasma. This substitution maintains flight stability capability while dramatically reducing weight and associated energy losses, thereby improving overall aircraft efficiency.

The invention uses periodic or pulsed plasma generation to provide stable control forces. By timing and modulating plasma activation patterns, the system achieves stable flight control without requiring continuous heavy mechanical structures, reducing energy consumption while maintaining stability.