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Optimal Transition of Coaxial Compound Helicopter after Total Propeller Failure
Publisher: American Society of Civil Engineers
Abstract: The research explores transition strategies of a coaxial compound helicopter transitioning to pure coaxial-rotor mode following a complete aft propeller failure. For that, a flight dynamics model is developed to predict ...
An Onboard Aeroengine Model-Tuning System
Publisher: American Society of Civil Engineers
Abstract: This study investigates an onboard aeroengine model (OBEM)-tuning system (OTS) based on a hybrid Kalman filter, which is mostly used to estimate the aeroengine performance. The OTS structure comprises two parts. One is an ...
Hybrid Diagnosis System for Aeroengine Sensor and Actuator Faults
Publisher: ASCE
Abstract: This paper presents a hybrid model-based fault diagnosis system to distinguish different types of faults and provide accurate fault information under complex fault situations. In the proposed system, a bank of hybrid fault ...
Automatic Pixel-Level Segmentation of Multiple Pavement Distresses and Surface Design Features with PDSNet II
Publisher: American Society of Civil Engineers
Abstract: Effective distress detection and quantitative analysis play a crucial role in road maintenance and driving safety. The Pavement distress segmentation network (PDSNet) is designed to combine the pyramid scene parsing network ...
Attaching Characteristics of the Natural Gas Jet Flame in Air-Coflow at Various Conditions
Publisher: American Society of Civil Engineers