2012 IEEE International Conference on Control Applications 2012
DOI: 10.1109/cca.2012.6402397
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State observer based robust feedback linearization controller for twin rotor MIMO system

Abstract: This paper presents, a state observer based controller for the twin rotor multiple-input-multiple-output (MIMO) system. The twin rotor MIMO system (TRMS) belongs to a class of nonlinear system having high coupling effect between two propellers, unstable and nonlinear dynamics. A state observer is designed using coordinate change which transforms the TRMS into an approximate normal form. Based on the proposed observer, a feedback linearization controller is designed for TRMS. The control effort is further compe… Show more

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Cited by 5 publications
(5 citation statements)
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“…If u 1 and u 2 are the input voltages for the DC motor of twin rotors and τ 1 and τ 2 are the respective output torques for the main and tail rotors, then the motor with mechanical characteristics and electrical control circuit is approximated by following the differential equations (Feedback, 2010; Pratap and Purwar, 2012; Ramalakshmi and Manoharan, 2012).…”
Section: Problem Formulationmentioning
confidence: 99%
See 3 more Smart Citations
“…If u 1 and u 2 are the input voltages for the DC motor of twin rotors and τ 1 and τ 2 are the respective output torques for the main and tail rotors, then the motor with mechanical characteristics and electrical control circuit is approximated by following the differential equations (Feedback, 2010; Pratap and Purwar, 2012; Ramalakshmi and Manoharan, 2012).…”
Section: Problem Formulationmentioning
confidence: 99%
“…The following TRMS dynamic model (Feedback, 2010; Pratap and Purwar, 2012; Ramalakshmi and Manoharan, 2012; Huang, 2011) for the mechanical unit can be derived.…”
Section: Problem Formulationmentioning
confidence: 99%
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“…Most of these controllers utilized the signum function in their designs to compensate for uncertainties ( [1] [15], [16]). Only a few results considered output feedback (i.e., only angular position information being available) ([11], [17], [18], [19]). The lack of accurate dynamic models and angular velocity measurements constituted the main motivation of this work.…”
Section: Introductionmentioning
confidence: 99%