Add to ORKGThe presentation describes a design procedure based on multi-objective genetic algorithms and a backward simulation tool named PLA.N.E.S. The input parameters were the size of engine and electric motor, the specification of the battery and the battery management strategy. The procedure was applied to an unmanned aerial vehicle. The goals of the optimisation were minimisation of fuel consumption, maximisation of electric endurance, minimisation of the powertrain volume and maximisation of the performance at takeoff
Hybrid aircraft is a new attempt for next-generation aircraft, they are environmentally friendly and...
The increasing demands for air-taxi operations together with the ambitious targets for reduced envir...
An integrated engine cycle design methodology and mission assessment for parallel hybrid electric pr...
Purpose – This paper addressed some critical issues in the development of hybrid electric powertrain...
Purpose The purpose of this study is to investigate the optimization of design and energy management...
The design of a hybrid electric powertrain requires a complex optimization procedure because its per...
As the aviation sector keeps expanding, a growing interest in technologies that can reduce the depen...
The complexity of hybrid-electric aircraft propulsion systems is also characterized by the greater n...
Currently fielded electric-powered small unmanned aircraft systems (UAS) lack the endurance desired ...
Hybrid electric aircraft have been proposed as a means to achieve the ambitious fuel burn reduction ...
Hybrid powerplants combining Internal Combustion Engines (ICE) and Electric Motor (EM) prime movers ...
The aviation world is dealing with the development of new and greener aviation. The need for reducin...
The interest in electric and hybrid electric power system has been increasing, in recent times, due ...
The aviation sector and its associated activities contribute to climate change, damage to the enviro...
Hybrid-electric civil airliners (HECAs) are considered the forerunner of the solution of relieving a...
Hybrid aircraft is a new attempt for next-generation aircraft, they are environmentally friendly and...
The increasing demands for air-taxi operations together with the ambitious targets for reduced envir...
An integrated engine cycle design methodology and mission assessment for parallel hybrid electric pr...
Purpose – This paper addressed some critical issues in the development of hybrid electric powertrain...
Purpose The purpose of this study is to investigate the optimization of design and energy management...
The design of a hybrid electric powertrain requires a complex optimization procedure because its per...
As the aviation sector keeps expanding, a growing interest in technologies that can reduce the depen...
The complexity of hybrid-electric aircraft propulsion systems is also characterized by the greater n...
Currently fielded electric-powered small unmanned aircraft systems (UAS) lack the endurance desired ...
Hybrid electric aircraft have been proposed as a means to achieve the ambitious fuel burn reduction ...
Hybrid powerplants combining Internal Combustion Engines (ICE) and Electric Motor (EM) prime movers ...
The aviation world is dealing with the development of new and greener aviation. The need for reducin...
The interest in electric and hybrid electric power system has been increasing, in recent times, due ...
The aviation sector and its associated activities contribute to climate change, damage to the enviro...
Hybrid-electric civil airliners (HECAs) are considered the forerunner of the solution of relieving a...
Hybrid aircraft is a new attempt for next-generation aircraft, they are environmentally friendly and...
The increasing demands for air-taxi operations together with the ambitious targets for reduced envir...
An integrated engine cycle design methodology and mission assessment for parallel hybrid electric pr...