2021
DOI: 10.1016/j.conengprac.2021.104806
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Observer-based fixed-time continuous nonsingular terminal sliding mode control of quadrotor aircraft under uncertainties and disturbances for robust trajectory tracking: Theory and experiment

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Cited by 73 publications
(57 citation statements)
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“…For the simulated and real-world experiments, PX4 [31] and DJI A3 controllers were employed, respectively. The second experiment was devoted to demonstrating the behaviour of the proposed approach in a real-world condition 3 , where the initial reference trajectory passes through a cluttered environment followed by open space and back to a cluttered environment where the terminal pose was placed in an obstacle zone. Map update range (update range) was kept 4m from the center of the MAV and max speed set to 0.6m/s for the safety of MAV.…”
Section: Experimental Procedures and Resultsmentioning
confidence: 99%
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“…For the simulated and real-world experiments, PX4 [31] and DJI A3 controllers were employed, respectively. The second experiment was devoted to demonstrating the behaviour of the proposed approach in a real-world condition 3 , where the initial reference trajectory passes through a cluttered environment followed by open space and back to a cluttered environment where the terminal pose was placed in an obstacle zone. Map update range (update range) was kept 4m from the center of the MAV and max speed set to 0.6m/s for the safety of MAV.…”
Section: Experimental Procedures and Resultsmentioning
confidence: 99%
“…Such a behaviour is due the 2 tracking accuracy without considering obstacles: https://www.youtube. com/watch?v=pKVeGdr8crU 3 behaviour of the proposed approach in a challenging environment https: //youtu.be/g6xHvkcrYcQ Fig. 7.…”
Section: Experimental Procedures and Resultsmentioning
confidence: 99%
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“…Проте у даних дослідженнях не враховані важливість зон території та ймовірність виявлення об'єктів у зонах, тобто території розглядаються як однор ідні. Відповідно до методології, що представлена у [5], термінальне упра вління рухом динамічних датчиків слід будувати поетапно. Насамперед необхідно побудувати просторову траєкторію руху центру мас літального апарата.…”
Section: аналіз сучасних досліджень та постановка проблемиunclassified