Modeling and PID Control of a Quadrotor Aerial Robot
This paper elucidates the modeling of a + quadrotor configuration aerial vehicle and the design of its attitude and altitude controllers. The aircraft model consists of four fixed pitch angle propeller, each driven by an electric DC motor. The hovering flight of the quadrotor is governed by the Newt...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
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Trans Tech Publications, Switzerland
2014
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| Subjects: | |
| Online Access: | http://umpir.ump.edu.my/id/eprint/5545/1/scan0011.pdf |
| _version_ | 1825821661310484480 |
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| author | Ismail, Mohd Khairuddin Anwar, P. P. A. Majeed Abdul Aziz, Jaafar Jessnor Arif, Mat Jizat |
| author_facet | Ismail, Mohd Khairuddin Anwar, P. P. A. Majeed Abdul Aziz, Jaafar Jessnor Arif, Mat Jizat |
| author_sort | Ismail, Mohd Khairuddin |
| collection | UMP |
| description | This paper elucidates the modeling of a + quadrotor configuration aerial vehicle and the design of its attitude and altitude controllers. The aircraft model consists of four fixed pitch angle propeller, each driven by an electric DC motor. The hovering flight of the quadrotor is governed by the Newton-Euler formulation. The attitude and altitude controls of the aircraft were regulated using heuristically tuned (Proportional-Integral-Derivative) PID controller. It was numerically simulated via Simulink that a PID controller was sufficient to bring the aircraft to the required altitude whereas the attitude of the vehicle is adequately controlled by a PD controller. |
| first_indexed | 2024-03-06T11:44:55Z |
| format | Article |
| id | UMPir5545 |
| institution | Universiti Malaysia Pahang |
| language | English |
| last_indexed | 2024-03-06T11:44:55Z |
| publishDate | 2014 |
| publisher | Trans Tech Publications, Switzerland |
| record_format | dspace |
| spelling | UMPir55452018-05-28T07:46:09Z http://umpir.ump.edu.my/id/eprint/5545/ Modeling and PID Control of a Quadrotor Aerial Robot Ismail, Mohd Khairuddin Anwar, P. P. A. Majeed Abdul Aziz, Jaafar Jessnor Arif, Mat Jizat TS Manufactures This paper elucidates the modeling of a + quadrotor configuration aerial vehicle and the design of its attitude and altitude controllers. The aircraft model consists of four fixed pitch angle propeller, each driven by an electric DC motor. The hovering flight of the quadrotor is governed by the Newton-Euler formulation. The attitude and altitude controls of the aircraft were regulated using heuristically tuned (Proportional-Integral-Derivative) PID controller. It was numerically simulated via Simulink that a PID controller was sufficient to bring the aircraft to the required altitude whereas the attitude of the vehicle is adequately controlled by a PD controller. Trans Tech Publications, Switzerland 2014 Article PeerReviewed application/pdf en http://umpir.ump.edu.my/id/eprint/5545/1/scan0011.pdf Ismail, Mohd Khairuddin and Anwar, P. P. A. Majeed and Abdul Aziz, Jaafar and Jessnor Arif, Mat Jizat (2014) Modeling and PID Control of a Quadrotor Aerial Robot. Advanced Materials Research, 903. pp. 327-331. ISSN 1022-6680 (print), 1662-8985 (online). (Published) http://www.scientific.net/AMR.903.327 DOI: 10.4028/www.scientific.net/AMR.903.327 |
| spellingShingle | TS Manufactures Ismail, Mohd Khairuddin Anwar, P. P. A. Majeed Abdul Aziz, Jaafar Jessnor Arif, Mat Jizat Modeling and PID Control of a Quadrotor Aerial Robot |
| title | Modeling and PID Control of a Quadrotor Aerial Robot |
| title_full | Modeling and PID Control of a Quadrotor Aerial Robot |
| title_fullStr | Modeling and PID Control of a Quadrotor Aerial Robot |
| title_full_unstemmed | Modeling and PID Control of a Quadrotor Aerial Robot |
| title_short | Modeling and PID Control of a Quadrotor Aerial Robot |
| title_sort | modeling and pid control of a quadrotor aerial robot |
| topic | TS Manufactures |
| url | http://umpir.ump.edu.my/id/eprint/5545/1/scan0011.pdf |
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