Design of a Flight Control System in Compliance with Fling and Handling Quality Requirements
نویسنده
چکیده
The un-augmented open loop 6-DOF Aerosonde exhibits poor stability and control characteristics in compliance with MIL-F8785C flying quality standards. As in most classical fixed wing aircrafts, the control inputs to Aerosonde result in pitch, roll and yaw rate responses (rate command characteristics). This has made manual trimming of the UAV, at a given flight condition, with a human pilot-operator closing the loop, a daunting task.
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