Kalman filter based modification on helicopter adaptive control

Date

2015-01-05

Author

Yavrucuk, İlkay

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In this paper, a Kalman Filter based e-modification term is used in the update law of an online learning adaptive neural network controller for a helicopter application. The controller is applied to a high fidelity helicopter simulation model. The applications include both an example on a single-input single-output controller structure using a linear in the parameter neural network, but also a multi-input multi-output neural network structure to compensate uncertainties in the attitude control of a helicopter. It is observed that using a Kalman Filter based e-modification provides improved command following and requires less control effort compared to traditional e-modification.

URI

https://hdl.handle.net/11511/88139

Conference Name

AIAA Scitech Conference, (5 - 09 Ocak 2015)

Collections

Department of Aerospace Engineering, Conference / Seminar

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Citation Formats

İ. Yavrucuk, “Kalman filter based modification on helicopter adaptive control,” presented at the AIAA Scitech Conference, (5 - 09 Ocak 2015), 2015, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/88139.