Controller design for RCTA aircraft using parameter estimation to integrate navigational technique

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Primary RJ20102023_merged_Roli.pdf (6.92 MB)

Date

2023-10

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School of Engineering, UPES, Dehradun

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Thesis submitted in partial fulfillment of the requirements for the award of the Degree of Doctor of Philosophy (Aerospace Engineering)

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Thesis, Aerospace Engineering, Aircraft System Identification, Flight control System Design, Aircraft Controller Design, Aircraft Navigation System, Research Cum Trainer Aircraft

Citation

Under the guidance of Dr. Om Prakash, Professor, UPES & Dr. Sudhir Kumar Chaturvedi, Associate Professor, UPES

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https://dr.ddn.upes.ac.in/handle/123456789/4309

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