The application discloses a center-of-gravity driving aircraft precise attitude regulation method and
system, and particularly relates to the field of aircraft
attitude control technology, and is used for solving the problem of high operation threshold and easy loss of control of man-
machine coupling in a complex environment. First, cabin pressure distribution data is collected and
frequency domain decoupling is performed, and a real low-frequency intention driving vector and an associated high-frequency
jitter feature are accurately separated. Then, the intention is mapped to a flow field coordinate
system that fuses
terrain and
airflow to perform aerodynamic interference impedance analysis, generate an aerodynamic impedance compensation matrix, and avoid collision risks. The high-frequency
jitter and the expected body
angular response matching
resonance band are extracted, a dynamic anti-oscillation damping coefficient is output, and
resonance is suppressed. Finally, multi-dimensional parameters are input into a
nonlinear control solver to perform joint optimization and generate a thrust distribution sequence for execution, thereby constructing a regulation
closed loop from intention decoupling to physical execution, and ensuring extreme smoothness and
flight safety in an extremely simple
operation mode.