Helicopter Integrated Flight/Propulsion Control Technology

摘要

Helicopter integrated flight/propulsion control (IFPC) is a large complex system. This paper applied a large system theory and established the helicopter IFPC integral model. The paper studied a dynamic response to collective controller of the integral control model in hovering condition of Black Hawk helicopter and effect on performance. The helicopter performance satisfied Handling Qualities Requirements for Military Rotorcraft (ADS-33D). Improved trend of the helicopter performance was obtained.