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

Simple item page
dc.contributor.authorJaiswal, Roli
dc.date.accessioned2024-09-18T12:23:07Z
dc.date.available2024-09-18T12:23:07Z
dc.date.issued2023-10
dc.descriptionThesis submitted in partial fulfillment of the requirements for the award of the Degree of Doctor of Philosophy (Aerospace Engineering)en_US
dc.identifier.citationUnder the guidance of Dr. Om Prakash, Professor, UPES & Dr. Sudhir Kumar Chaturvedi, Associate Professor, UPESen_US
dc.identifier.urihttps://dr.ddn.upes.ac.in/handle/123456789/4309
dc.language.isoenen_US
dc.publisherSchool of Engineering, UPES, Dehradunen_US
dc.subjectThesisen_US
dc.subjectAerospace Engineeringen_US
dc.subjectAircraft System Identificationen_US
dc.subjectFlight control System Designen_US
dc.subjectAircraft Controller Designen_US
dc.subjectAircraft Navigation Systemen_US
dc.subjectResearch Cum Trainer Aircraften_US
dc.titleController design for RCTA aircraft using parameter estimation to integrate navigational techniqueen_US
dc.typeThesisen_US

Files

Original bundle

Now showing 1 - 1 of 1
Thumbnail Image
Name:
RJ20102023_merged_Roli.pdf
Size:
6.92 MB
Format:
Adobe Portable Document Format
Description:
Download

License bundle

Now showing 1 - 1 of 1
Thumbnail Image
Name:
license.txt
Size:
1.71 KB
Format:
Item-specific license agreed upon to submission
Description:
Download

Collections

Thesis