| 摘要 |
PURPOSE: An unmanned aerial vehicle control system designing method is provided to obtain a control gain suitable for a designer by applying a parameter optimization technique even though controller structure is changed. CONSTITUTION: A designing reference point is determined through designing information which a designer inputs(S100). A linear flight is performed through fine control of an unmanned aerial vehicle in a designing flight condition(S200). Controller structure is designed(S300). Automatic piloting device structure suitable for the designed controller structure is designed(S400). Performance of a control system designed by the automatic piloting device structure is verified(S500). Whether a result of the verified performance is good is determined(S600). [Reference numerals] (AA) Start; (BB) End; (S100) Determining a designing reference point; (S200) Trim and linearization step in a flight condition; (S300) Designing controller structure; (S400) Designing automatic operating device structure; (S500) Verifying designed control system performance; (S600) Performance is good?; (S700) Controller structure problem?; (S800) Comparing a linear simulation and a result; (S900) In error range? |
