Faults or failures are inevitable to occur and their prompt detection and isolation are
essential for the dependability of various systems and for avoiding damages to the system …

This work analyzes the effects of variable operating rotor speed on the helicopter low-speed
Height–Velocity (HV) diagram in one engine inoperative (OEI) situation. Using the UH-60A …

An augmented flight dynamics model is developed to extend the existing flight dynamics
model of tilt-rotor aircraft for optimal landing procedure analysis in the event of one engine …

This paper presents a method to predict the pilot workload in helicopter landing after one
engine failure. The landing procedure is simulated numerically via applying nonlinear …

This paper focuses on the prediction of the safe autorotation landing operations of a
helicopter following engine failure. The autorotation landing procedure is formulated as a …

This paper studies the control strategy in tilt-rotor aircraft dynamic conversion procedure. A
nonlinear flight dynamics model with full flight modes is established. On this basis, a …

The design of a high-performance guidance and control system for a small-scale
helicopterUnmanned Aerial Vehicle (UAV), with an engine OFF flight condition (ie …

(57) ABSTRACT A method of automating entry of an aircraft into autorotation includes
detecting a loss of engine power, analyzing a sensed height and sensed airspeed of the …

This paper focuses on the optimal takeoff of a coaxial compound helicopter, considering the
possibility of engine failure. When one engine fails during takeoff, a twin-engine helicopter …

This paper investigates the optimal landing trajectory and control procedure when a
helicopter undergoes autorotation due to tail rotor drive failure (TRDF), in which an optimal …