Proportional Derivative Active Force Control for “X” Configuration Quadcopter
<p>This paper present a control method “x” configuration quadcopter. The control method used PDAFC (Proportional Derivative Active Force Control). PD is used to stabilize quadcopter, and AFC is used to reject uncertainty disturbance (e.g. wind) by estimate disturbance torque value of quadcopte...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
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Indonesian Institute of Sciences
2014-12-01
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| Series: | Journal of Mechatronics, Electrical Power, and Vehicular Technology |
| Subjects: | |
| Online Access: | http://mevjournal.com/index.php/mev/article/view/178 |
| _version_ | 1818159873064435712 |
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| author | Niam Tamami Endra Pitowarno I Gede Puja Astawa |
| author_facet | Niam Tamami Endra Pitowarno I Gede Puja Astawa |
| author_sort | Niam Tamami |
| collection | DOAJ |
| description | <p>This paper present a control method “x” configuration quadcopter. The control method used PDAFC (Proportional Derivative Active Force Control). PD is used to stabilize quadcopter, and AFC is used to reject uncertainty disturbance (e.g. wind) by estimate disturbance torque value of quadcopter. By adding PD with AFC, better result is obtained, AFC can minimize uncertainty disturbance effect. The sensitivity toward uncertainty disturbance can be set from sensitivity constant to get best performance of disturbance rejection. Stability analysis of PDAFC was evaluated by Lyapunov stability theory.</p> |
| first_indexed | 2024-12-11T15:52:54Z |
| format | Article |
| id | doaj.art-2857937abf894a7c9983c0bb771946e5 |
| institution | Directory Open Access Journal |
| issn | 2087-3379 2088-6985 |
| language | English |
| last_indexed | 2024-12-11T15:52:54Z |
| publishDate | 2014-12-01 |
| publisher | Indonesian Institute of Sciences |
| record_format | Article |
| series | Journal of Mechatronics, Electrical Power, and Vehicular Technology |
| spelling | doaj.art-2857937abf894a7c9983c0bb771946e52022-12-22T00:59:31ZengIndonesian Institute of SciencesJournal of Mechatronics, Electrical Power, and Vehicular Technology2087-33792088-69852014-12-0152677410.14203/j.mev.2014.v5.67-74101Proportional Derivative Active Force Control for “X” Configuration QuadcopterNiam Tamami0Endra Pitowarno1I Gede Puja Astawa2Electronics Engineering Polytechnic Institute of SurabayaElectronics Engineering Polytechnic Institute of SurabayaElectronics Engineering Polytechnic Institute of Surabaya<p>This paper present a control method “x” configuration quadcopter. The control method used PDAFC (Proportional Derivative Active Force Control). PD is used to stabilize quadcopter, and AFC is used to reject uncertainty disturbance (e.g. wind) by estimate disturbance torque value of quadcopter. By adding PD with AFC, better result is obtained, AFC can minimize uncertainty disturbance effect. The sensitivity toward uncertainty disturbance can be set from sensitivity constant to get best performance of disturbance rejection. Stability analysis of PDAFC was evaluated by Lyapunov stability theory.</p>http://mevjournal.com/index.php/mev/article/view/178“x”quadcopterstabilityPDAFC |
| spellingShingle | Niam Tamami Endra Pitowarno I Gede Puja Astawa Proportional Derivative Active Force Control for “X” Configuration Quadcopter Journal of Mechatronics, Electrical Power, and Vehicular Technology “x” quadcopter stability PD AFC |
| title | Proportional Derivative Active Force Control for “X” Configuration Quadcopter |
| title_full | Proportional Derivative Active Force Control for “X” Configuration Quadcopter |
| title_fullStr | Proportional Derivative Active Force Control for “X” Configuration Quadcopter |
| title_full_unstemmed | Proportional Derivative Active Force Control for “X” Configuration Quadcopter |
| title_short | Proportional Derivative Active Force Control for “X” Configuration Quadcopter |
| title_sort | proportional derivative active force control for x configuration quadcopter |
| topic | “x” quadcopter stability PD AFC |
| url | http://mevjournal.com/index.php/mev/article/view/178 |
| work_keys_str_mv | AT niamtamami proportionalderivativeactiveforcecontrolforxconfigurationquadcopter AT endrapitowarno proportionalderivativeactiveforcecontrolforxconfigurationquadcopter AT igedepujaastawa proportionalderivativeactiveforcecontrolforxconfigurationquadcopter |