COMBINED MODEL-REFERENCE ADAPTIVE CONTROLLER FOR COORDINATED TURN OF A TAILLESS AIRCRAFT

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NAVABI MOHAMMAD; KAKAVAND ESMAEEL

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Journal: Modares Mechanical Engineering Year:2016 | Volume:15 | Issue:10 Page(s): 117-127

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Information Journal Paper

Title

COMBINED MODEL-REFERENCE ADAPTIVE CONTROLLER FOR COORDINATED TURN OF A TAILLESS AIRCRAFT

Author(s)

NAVABI MOHAMMAD | KAKAVAND ESMAEEL | Issue Writer Certificate

Keywords

MODEL-REFERENCE ADAPTIVE CONTROLLERQ1

COMBINED ERRORQ2

COORDINATED TURN MANEUVERQ2

TAILLESS AIRCRAFTQ2

PARAMETRIC AND NON-PARAMETRICQ2

UNCERTAINTIESQ2

Abstract

Due to instability and specific configuration of TAILLESS AIRCRAFT, there should be a controller with capability of stabilizing the aircraft in various maneuvers and flight conditions and also to have desired robustness against different PARAMETRIC AND NON-PARAMETRIC UNCERTAINTIES. In this paper, we design a multi input-multi output combined MODEL-REFERENCE ADAPTIVE CONTROLLER for a TAILLESS AIRCRAFT. Coordinated turn is itself an unstable maneuver. The addition of the instability of this maneuver and the instability of a TAILLESS AIRCRAFT causes a highly unstable situation. Combined model-reference adaptive control benefits the aggregation of the tracking error and prediction error. Combining these two sources of errors alleviates the transient response characteristics, and a combined MODEL-REFERENCE ADAPTIVE CONTROLLER has better performance compared to the classical MODEL-REFERENCE ADAPTIVE CONTROLLERs (with tracking error as the only source of parameter estimation error), and this property could be useful in highly unstable systems like TAILLESS AIRCRAFT. Here, after extracting the equations of motion of an aircraft and exerting the conditions of COORDINATED TURN MANEUVER, we design a combined MODEL-REFERENCE ADAPTIVE CONTROLLER for a TAILLESS AIRCRAFT. The simulation results show accuracy of the designed controller in stabilizing the aircraft during the COORDINATED TURN MANEUVER and its robustness against UNCERTAINTIES.

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APA: Copy

NAVABI, MOHAMMAD, & KAKAVAND, ESMAEEL. (2016). COMBINED MODEL-REFERENCE ADAPTIVE CONTROLLER FOR COORDINATED TURN OF A TAILLESS AIRCRAFT. MODARES MECHANICAL ENGINEERING, 15(10), 117-127. SID. https://sid.ir/paper/179622/en

Vancouver: Copy

NAVABI MOHAMMAD, KAKAVAND ESMAEEL. COMBINED MODEL-REFERENCE ADAPTIVE CONTROLLER FOR COORDINATED TURN OF A TAILLESS AIRCRAFT. MODARES MECHANICAL ENGINEERING[Internet]. 2016;15(10):117-127. Available from: https://sid.ir/paper/179622/en

IEEE: Copy

MOHAMMAD NAVABI, and ESMAEEL KAKAVAND, “COMBINED MODEL-REFERENCE ADAPTIVE CONTROLLER FOR COORDINATED TURN OF A TAILLESS AIRCRAFT,” MODARES MECHANICAL ENGINEERING, vol. 15, no. 10, pp. 117–127, 2016, [Online]. Available: https://sid.ir/paper/179622/en

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