一种重心驱动的飞行器精准姿态调控方法及系统
By analyzing the spatiotemporal gradient and decoupling the frequency domain of the pressure distribution in the aircraft cabin, and combining aerodynamic impedance analysis and nonlinear control, an aerodynamic impedance compensation matrix is generated. This solves the problems of aircraft control complexity and emergency response hysteresis, and enables stable and safe flight in complex aerodynamic environments.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- KUFEI (ZHEJIANG) AIRCRAFT TECHNOLOGY CO LTD
- Filing Date
- 2026-05-09
- Publication Date
- 2026-07-17
AI Technical Summary
Existing aircraft control methods have steep learning curves, slow emergency response, and are prone to human-machine coupling oscillations in complex aerodynamic environments, leading to attitude instability and making it difficult to achieve minimalist control and safe flight.
By acquiring the time-series matrix of cabin pressure distribution, performing spatiotemporal gradient analysis and frequency domain decoupling, extracting the low-frequency intention driving vector of the occupants and mapping it to the local flow field coordinate system for aerodynamic interference impedance analysis, generating an aerodynamic impedance compensation matrix, and combining it with a nonlinear control solver to generate a multi-rotor thrust distribution sequence, thereby achieving precise attitude control.
It effectively filters out physiological tremors of occupants, predicts aerodynamic stall and collision risks, suppresses human-machine coupling resonance, and achieves stability and safety of the aircraft in complex environments.
Smart Images
Figure CN122151908B_ABST