2020 American Control Conference (ACC) 2020
DOI: 10.23919/acc45564.2020.9147794
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Quaternion Feedback Based Autonomous Control of a Quadcopter UAV with Thrust Vectoring Rotors

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Cited by 15 publications
(3 citation statements)
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“…Furthermore, it can be argued that more conservative acceleration profiles lead to an increased power efficiency. This assumption can be done by looking at Equation 3, which relates the required thrust to the linear acceleration, as shown in (Kumar et al, 2020).…”
Section: Experiments and Resultsmentioning
confidence: 99%
“…Furthermore, it can be argued that more conservative acceleration profiles lead to an increased power efficiency. This assumption can be done by looking at Equation 3, which relates the required thrust to the linear acceleration, as shown in (Kumar et al, 2020).…”
Section: Experiments and Resultsmentioning
confidence: 99%
“…The quaternion representation is used to avoid problems associated to the gimbal lock [39]. Then, the normalised orientation quaternion…”
Section: B Orientation Estimationmentioning
confidence: 99%
“…The mathematical dynamic modeling of the tilt-rotor UAV are discussed in [17]. The PD based control methods and non-linear sliding mode controller design for the tilt-rotor UAV were studied in [18,19,20]. This system has also been described as capable of handling single motor failure during flight [19].…”
Section: Introductionmentioning
confidence: 99%