2019
DOI: 10.1061/(asce)as.1943-5525.0001005
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Degraded Planary Tracking Control of an Omnidirectional Vectored-Thruster Aerostat

Abstract: The problem of horizontal-plane tracking control of an omni-directional, four vectored-thruster aerostat when subjected to actuator failure is considered. The actuator failures result in the aerostat becoming underactuated, so it can only effect surge force and pure yaw moment about the body centre. To achieve accurate position control in the horizontal plane, direct position control is used instead of heading control.This mode of controller is called degraded tracking control in contrast to full authority con… Show more

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Cited by 2 publications
(2 citation statements)
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“…If we assume slight excursions in the roll, pitch, yaw, and heave, then the simplified horizontal plane 2-DOF dynamics used for the controller design are described by 27 (m + m 11 ) _ u = (m + m 22 )vr +…”
Section: Simulation Resultsmentioning
confidence: 99%
See 1 more Smart Citation
“…If we assume slight excursions in the roll, pitch, yaw, and heave, then the simplified horizontal plane 2-DOF dynamics used for the controller design are described by 27 (m + m 11 ) _ u = (m + m 22 )vr +…”
Section: Simulation Resultsmentioning
confidence: 99%
“…External forces and moments are induced by gravity, buoyancy, fluid inertia force, aerodynamics, and thrusters. The following dynamics equation can be constructed in the body-fixed frame through force analysis 26 , 27 :…”
Section: Application To a Multi-vectored Propeller Airship Modelmentioning
confidence: 99%