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      Analysis of Stability, Response and LQR Controller Design of a Small Scale Helicopter Dynamics

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          Abstract

          This paper presents how to use feedback controller with helicopter dynamics state space model. A simplified analysis is presented for controller design using LQR of small scale helicopters for axial and forward flights. Our approach is simple and gives the basic understanding about how to develop controller for solving the stability of linear helicopter flight dynamics.

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          Author and article information

          Journal
          30 April 2008
          Article
          0804.4757
          af5a37d7-4fdc-46fa-b73a-ca7fcf1cdb33

          http://arxiv.org/licenses/nonexclusive-distrib/1.0/

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          Proceedings of the International Conference on Intelligent Unmanned System (ICIUS 2007), Bali, Indonesia, October 24-25, 2007, Paper No. ICIUS2007-C006
          Uploaded by ICIUS2007 Conference Organizer on behalf of the author(s). 8 pages, 19 figures, 4 tables
          cs.RO

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