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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1989, Vol. 10 ›› Issue (8): 381-388.

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THE OPTIMUM CONTROL AND ADAPTIVE CONTROL FOR AIRPLANE CABIN PRESSURE

Ying Wenjiang   

  1. Nanjing Aeronautial Institute
  • Received:1988-01-28 Revised:1900-01-01 Online:1989-08-25 Published:1989-08-25

Abstract:

This paper presents a new design for airplane cabin pressure, i.e. the optimum and adaptive control for airplane cabin pressure. A new scheme, design method and formulas of this control system are derived by means of the application of the modern control theory.

Key words: optimum control, adaptive, control cabin pressure, pressure regulator