Unmanned aerial vehicles (UAV) and other similar mechatronics systems will uses the servomechanisms for the accurate positioning of construction elements here it is stable, reliable and easy to control.The Improvement of Power Distribution system for UAV mainly depends on Mechatronic system reliability; aerospace safety; servomechanisms; short‐circuit protection.Most of the UAVs are developed without such analysis because it is considered as a normal electrical, electronic and electro‐ mechanic component.it does not apply to major aerospace companies that strictly adhere to engineering standards and this method is only applicable for the UAV control system which improves the reliability and fault tolerance of commercial products.
In certain rare environmental cases that the components may get failed and thus it leads the operations of the entire system to fail.Improvement of Power Distribution system for UAV having the boost converter to a fixed DC bus, the decreased efficiency and maximum flight-time compared to the conventional approach of the DC bus voltage varying with battery voltage. The DC-DC converter requires more craft thrust and thus an increase in craft output power in addition to the increased losses. The non-critical servomechanisms could be considered the flaps, rudder in case of malfunction of the flap servomechanisms and it would be preferable to deactivate the mechanism on the other side of a wing to avoid asymmetrical takeoff.Here the overcurrent protection should be provided for the dynamically variable load; the peak,short term and long‐term overcurrent should be evaluated, and different protection scenarios could be used to realize the power distribution fault tolerance system, and tokeeping the maximum available level of UAV operation.
ALGORITHM AND ITS FUNCTIONS: