An aircraft cabin temperature adaptive control system based on predictive control
By using an adaptive control system based on predictive control, the problems of accuracy and response speed in cabin temperature control of aircraft have been solved. This system achieves high precision, rapid response and adaptive capability in cabin temperature control, extends the mechanical life of valves, and improves cabin comfort and safety.
Patent Information
- Authority / Receiving Office
- CN Β· China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
- Filing Date
- 2026-04-22
- Publication Date
- 2026-07-21
AI Technical Summary
Existing aircraft cabin temperature control systems cannot effectively handle cabin aging, changes in crew distribution, and non-uniform heat flow disturbances, resulting in decreased control accuracy and affecting valve mechanical lifespan. Furthermore, they have limited ability to handle sensor noise and unmodeled heat sources.
An adaptive control system based on predictive control is adopted. Noise is filtered out by a state cleaning module, a model wake-up module updates the high-dimensional predictive model, a prediction module optimizes the control sequence, and an execution module ensures that the temperature trajectory is within a safe range. Sensor noise and unmodeled heat sources are processed by combining high- and low-frequency fusion methods and orthogonal projection mechanisms.
It achieves high precision, rapid response, and adaptive capability for cabin temperature control, extends the mechanical life of valves, and improves cabin comfort and safety.
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Figure CN122064154B_ABST