A Review of Electric Actuation and Flight Control System for More/All Electric Aircraft

In recent decades, the aviation industry has made remarkable progress based on the development of different types of aircraft. Recent aircraft have begun to employ a large number of electrically powered equipment, as in the case of electric vehicles. These aircraft are referred to as M/AEA (More/All Electric Aircraft), and for civil aircraft, Boeing 787 and Airbus 380, began to apply these technologies significantly. Current aircrafts are being replaced by electrically powered equipment without the use of engine bleed air, which is the main source of secondary power, hydraulic systems and pneumatic pressure. This not only simplifies aircraft design and reduces weight, but also improves engine efficiency, making it an eco-friendly aircraft that improves fuel consumption and reduces pollutant emissions. In this paper, the author gave an overview and review electrically driven subsystems and flight control systems for M/AEA.