1994
DOI: 10.1109/48.338385
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The NDRE-AUV flight control system

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Cited by 158 publications
(61 citation statements)
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“…The decoupled control design procedure can be found in [5]. Healey and Marco [8], Healey and Lienard [7], Jalving [6] and others suggest that the 6 DOF linear equations of motion can be divided into three non-interacting (or lightly interacting) subsystems, grouping certain key motion equations together for the separate function of speed, steering and diving control. Each system consists of the state variables:…”
Section: Sliding Mode Autopilot Designmentioning
confidence: 99%
“…The decoupled control design procedure can be found in [5]. Healey and Marco [8], Healey and Lienard [7], Jalving [6] and others suggest that the 6 DOF linear equations of motion can be divided into three non-interacting (or lightly interacting) subsystems, grouping certain key motion equations together for the separate function of speed, steering and diving control. Each system consists of the state variables:…”
Section: Sliding Mode Autopilot Designmentioning
confidence: 99%
“…For flight-style operation, stern planes are used to adjust the pitch angle of the vehicle which in turn results in depth changes. A controller for flight-style operation may be designed based on a cascaded depth and pitch control structure [8,9,10,11,12]. In contrast, the control problem for hover-style operation may be considered as two parts [13,14,15].…”
Section: Introductionmentioning
confidence: 99%
“…In multiple articles (e.g. Zeng & Allen, 2004;Jalving, 1994) three different controllers are designed. One is used to control the speed, the other for the heading and the last one for the depth.…”
Section: Controls and Navigationmentioning
confidence: 99%