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Suradet Tantrairatn. Modelling and attitude control for tiltrotor UAV during transition flight mode. (). King Mongkut's University of Technology North Bangkok. Central Library. : , 2019.
Modelling and attitude control for tiltrotor UAV during transition flight mode
Name: Sarul Sakulthong
Organization :
Suranaree University of Technology. Department of Mechanical Engineering
Name: Suradet Tantrairatn
Organization :
Suranaree University of Technology. Department of Mechanical Engineering
Email :
suradetj@sut.ac.th
Name: Suradet Tantrairatn
Organization :
Suranaree University of Technology. Department of Mechanical Engineering
LCSH:
Drone aircraft
-- Control
Abstract:
Tiltrotor UAV is unmanned aerial vehicle which can take off and land vertically like helicopter and fly forward like a conventional fixed wing airplane. This process is called transition, tilting its rotors from vertical to horizontal and vice versa, which is the most critical flight mode due to its varying dynamics. This paper aims to present methodologies of designing control system for tiltrotor UAV, start with dynamic modelling. Model validation was done by comparing responses between flight test data and simulation in MATLAB Simulink. Then model reference adaptive control (MRAC) was designed and applied to adjust PID gains based on error between actual responses and responses from reference model for this tiltrotor UAV to control attitude roll and pitch response. Throughout transition flight mode, tiltrotor UAV can fly safely and able to stabilize itself along the flight
King Mongkut's University of Technology North Bangkok. Central Library
Address:
BANGKOK
Email:
library@kmutnb.ac.th
Created:
2019
Modified:
2020-08-11
Issued:
2020-08-11
บทความ/Article
application/pdf
BibliograpyCitation :
In Suranaree University of Technology The School of Mechanical Engineering Institute of Engineering. The 10th TSME International Conference on Mechanical Engineering 2019 (TSME-ICoME10) (p.267-273.). Pattaya : Department of Mechanical Engineering
eng
©copyrights King Mongkut's University of Technology North Bangkok
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0.029814 วินาที
Sarul Sakulthong
| Title | Contributor | Type |
|---|---|---|
| Modelling and attitude control for tiltrotor UAV during transition flight mode
มหาวิทยาลัยเทคโนโลยีพระจอมเกล้าพระนครเหนือ Sarul Sakulthong;Suradet Tantrairatn;Suradet Tantrairatn | บทความ/Article |
Suradet Tantrairatn
| Title | Contributor | Type |
|---|---|---|
| Modelling and attitude control for tiltrotor UAV during transition flight mode
มหาวิทยาลัยเทคโนโลยีพระจอมเกล้าพระนครเหนือ Sarul Sakulthong;Suradet Tantrairatn;Suradet Tantrairatn | บทความ/Article | |
| Frequency response system identification and flight controller tuning for quadcopter UAV
มหาวิทยาลัยเทคโนโลยีพระจอมเกล้าพระนครเหนือ Sarul Sakulthong;Suradet Tantrairatn;Watcharapol Saengphet | บทความ/Article |
Suradet Tantrairatn
| Title | Contributor | Type |
|---|---|---|
| Modelling and attitude control for tiltrotor UAV during transition flight mode
มหาวิทยาลัยเทคโนโลยีพระจอมเกล้าพระนครเหนือ Sarul Sakulthong;Suradet Tantrairatn;Suradet Tantrairatn | บทความ/Article | |
| Frequency response system identification and flight controller tuning for quadcopter UAV
มหาวิทยาลัยเทคโนโลยีพระจอมเกล้าพระนครเหนือ Sarul Sakulthong;Suradet Tantrairatn;Watcharapol Saengphet | บทความ/Article |