Engine condition monitoring on small single engine turboprop
Improving the port selection process during military deployments
Aerodynamic design of an electronics pod to maximise its carriage envelope on a fast-jet aircraft
The use of FEA and semi-empirical equations for weight estimation of a passenger aircraft
Safety performance functions to predict separation minima infringements in en-route airspace
Analysis of longitudinal dynamic stability of tandem wing aircraft
Design of hybrid electric heavy fuel MALE ISR UAV enabling technologies for military operations
Impact of actuators backlash on the helicopter control during landing on the moving vessel deck
Optimal energy management for hybrid-electric aircraft
A new simplified fluid dynamic model for digital twins of electrohydraulic servovalves
Modified vector field and nonlinear guidance law for low-cost UAV path following
Development process for preliminary aircraft sizing methods with regard to new technologies