Add to ORKGStarting an aircraft engine with an electrical machine has been one of the major trends for future aircraft. This paper studies the stability of a permanent-magnet machine (PMM) based aircraft starter/generator (S/G) system. Using control-to-output transfer functions, the stability analysis of this S/G system is thoroughly studied. The impact of the key parameters including the control parameters is analysed. Simulation and experimental results support the analytical result
This study describes the design, construction, and testing of an aero-engine starter-generator and i...
More-electric aircraft (MEA) has become a dominant trend for modern aircraft. On-board MEA, many fun...
Most loads of electrical power systems on a more electric aircraft (MEA) are regulated power convert...
The paper presents control analysis and design for a Permanent Magnet Machine (PMM) operated in Flux...
This paper presents control analysis and design for an aircraft electric starter-generator system ba...
More Electrical Aircraft (MEA) which replaces the hydraulic and pneumatic power by electrical power ...
The future aircraft electrical power system is expected to be more efficient, safer, simpler in serv...
A control approach for aircraft Starter/Generator (S/G) with Permanent Magnet Machine (PMM) operatin...
More Electric Aircraft (MEA) underline the utilization of electrical power to power the traditional ...
The trend towards development of More Electric Aircraft (MEA) has been driven by increased fuel foss...
This paper proposes an electric powertrain architecture for future hybrid electric aircrafts which s...
The more-electric aircraft concept is a major trend in aircraft electrical power system engineering ...
The concept of the More Electric Aircraft (MEA) is aimed at electrifying the mechanical, hydraulic, ...
The More-Electric Aircraft (MEA) concept is a major trend in aircraft electrical power system engine...
Development towards More Electric Aircraft (MEA) witnessed increase of electrical power source syste...
This study describes the design, construction, and testing of an aero-engine starter-generator and i...
More-electric aircraft (MEA) has become a dominant trend for modern aircraft. On-board MEA, many fun...
Most loads of electrical power systems on a more electric aircraft (MEA) are regulated power convert...
The paper presents control analysis and design for a Permanent Magnet Machine (PMM) operated in Flux...
This paper presents control analysis and design for an aircraft electric starter-generator system ba...
More Electrical Aircraft (MEA) which replaces the hydraulic and pneumatic power by electrical power ...
The future aircraft electrical power system is expected to be more efficient, safer, simpler in serv...
A control approach for aircraft Starter/Generator (S/G) with Permanent Magnet Machine (PMM) operatin...
More Electric Aircraft (MEA) underline the utilization of electrical power to power the traditional ...
The trend towards development of More Electric Aircraft (MEA) has been driven by increased fuel foss...
This paper proposes an electric powertrain architecture for future hybrid electric aircrafts which s...
The more-electric aircraft concept is a major trend in aircraft electrical power system engineering ...
The concept of the More Electric Aircraft (MEA) is aimed at electrifying the mechanical, hydraulic, ...
The More-Electric Aircraft (MEA) concept is a major trend in aircraft electrical power system engine...
Development towards More Electric Aircraft (MEA) witnessed increase of electrical power source syste...
This study describes the design, construction, and testing of an aero-engine starter-generator and i...
More-electric aircraft (MEA) has become a dominant trend for modern aircraft. On-board MEA, many fun...
Most loads of electrical power systems on a more electric aircraft (MEA) are regulated power convert...