The main objective of this project is to study and develop a novel morphing system which integrates up to four different morphing mechanisms into in a single wing and to demonstrate this new ability in flight. This system takes advantage of all the performance improvements achieved by adopting its wing shape according to the mission requirements of each flight phase. Therefore, this project envisions mitigating the required energy (and thus fuel consumption) to maintain the aircraft's flight and to perform the necessary flight maneuvers by offering the capacity to mould the exterior of the aircraft in order to enhance the necessary aspect of flight so as to lessen the required energy, such as lift over drag ratio, efficiency in aerodynamic control, lower stall velocity or to change to a better platform to perform a required maneuver.