Thats a unique idea.You should consider the following idea to enhance your idea so that it would impact uniquely: The dangers of poor pilot performance as ll as time and place conditions, low altitude and climate, damage critical aircraft control system. The use of Unmanned Aircraft Vehicle or (UAV) in sensitive and important Operation is required and there is a need for autopilot that can tune the MAV in different environment conditions. Furthermore, designing the controller system is one of the main discussed Dynamic issues in Flying Objects.  an attempted is made to determine the optimal coefficients of PID controller that can reject disturbances and still operate the MAV in stable positions. Basic PID controller is designed and is adopted to control the MAV, a modified techniques incorporating ISA-PID is designed to reject disturbances. The PID parameters are determined to be reduce the rise time less than 3 seconds, settling time to be less than 8 seconds and overshoot to be less than 5%. The developed model is suitable for PID controller in autopilot.
['Xuhui Chen', 'Ejaz Ul Haq', 'Jiawei Lin']
I am writing a research paper on a idea Design, modeling and tuning of modified PID controller for autopilot in MAVs
[{"from": "human", "value": "I am writing a research paper on a idea Design, modeling and tuning of modified PID controller for autopilot in MAVs"}, {"from": "gpt", "value": "Thats a unique idea.You should consider the following idea to enhance your idea so that it would impact uniquely: The dangers of poor pilot performance as ll as time and place conditions, low altitude and climate, damage critical aircraft control system. The use of Unmanned Aircraft Vehicle or (UAV) in sensitive and important Operation is required and there is a need for autopilot that can tune the MAV in different environment conditions. Furthermore, designing the controller system is one of the main discussed Dynamic issues in Flying Objects.  an attempted is made to determine the optimal coefficients of PID controller that can reject disturbances and still operate the MAV in stable positions. Basic PID controller is designed and is adopted to control the MAV, a modified techniques incorporating ISA-PID is designed to reject disturbances. The PID parameters are determined to be reduce the rise time less than 3 seconds, settling time to be less than 8 seconds and overshoot to be less than 5%. The developed model is suitable for PID controller in autopilot."}]