Partial linearization of the PVTOL aircraft with internal stability

被引：0
|
作者：
Lechappe, V. [1 ]
Aoustin, Y. [1 ]
Marquez-Martinez, L. A. [2 ]
Moog, C. H. [1 ]
机构：
[1] Univ Nantes, Ecole Cent Nantes, UMR CNRS 6597, LUNAM IRCCyN, F-44035 Nantes, France
[2] CICESE Res Ctr Ensenada BC Mexico, Ensenada, Baja California, Mexico
来源：
2013 IEEE 52ND ANNUAL CONFERENCE ON DECISION AND CONTROL (CDC) | 2013年
关键词：
nonlinear; MIMO; underactuated; non-minimum phase; zero-dynamics; internal dynamics; algebraic method; partial linearization; stabilization; PVTOL; NONLINEAR CONTROL DESIGN; STABILIZATION;
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
The planar vertical take-off and landing (PVTOL) aircraft is worked out by inspecting the various feedback linearization solutions. Partial linearizations of the state space are performed, which ensure the stability of the associated internal dynamics. The results are obtained through the search of dummy outputs with a 0-dimensional, 1-dimensional or 2-dimensional zero-dynamics that are stable.
引用
收藏
页码：2564 / 2569
页数：6
相关论文
共 50 条
  • [41] Control strategy using vision for the stabilization of an experimental PVTOL aircraft setup
    Palomino, A
    Castillo, P
    Fantoni, I
    Lozano, R
    Pégard, C
    IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2005, 13 (05) : 847 - 850
  • [42] Nonlinear control of the PVTOL aircraft by numerical inversion of its behavioral model
    Huu Phuc Nguyen
    De Miras, Jerome
    Bonnet, Stephane
    Charara, Ali
    2014 IEEE CONFERENCE ON CONTROL APPLICATIONS (CCA), 2014, : 457 - 462
  • [43] Global stabilisation of the PVTOL aircraft with lateral force coupling and bounded inputs
    Lopez-Araujo, D. J.
    Zavala-Rio, A.
    Fantoni, I.
    Salazar, S.
    Lozano, R.
    INTERNATIONAL JOURNAL OF CONTROL, 2010, 83 (07) : 1427 - 1441
  • [44] Output-Feedback Stabilization of the PVTOL Aircraft System Based on an Exact Differentiator
    Aguilar-Ibanez, Carlos
    Suarez-Castanon, Miguel S.
    Mendoza-Mendoza, Julio
    de Jesus Rubio, Jose
    Carlos Martinez-Garcia, Juan
    JOURNAL OF INTELLIGENT & ROBOTIC SYSTEMS, 2018, 90 (3-4) : 443 - 454
  • [45] Global stabilization of the PVTOL: real-time application to a mini-aircraft
    Lozano, R
    Castillo, P
    Dzul, A
    INTERNATIONAL JOURNAL OF CONTROL, 2004, 77 (08) : 735 - 740
  • [46] Output-Feedback Stabilization of the PVTOL Aircraft System Based on an Exact Differentiator
    Carlos Aguilar-Ibañez
    Miguel S. Suarez-Castanon
    Julio Mendoza-Mendoza
    Jose de Jesus Rubio
    Juan Carlos Martínez-García
    Journal of Intelligent & Robotic Systems, 2018, 90 : 443 - 454
  • [47] Robust constrained trajectory tracking control for a PVTOL aircraft subject to external disturbances
    Yao, Qijia
    INTERNATIONAL JOURNAL OF SYSTEMS SCIENCE, 2021, 52 (12) : 2617 - 2629
  • [48] APPLICATION OF LINEARIZATION ANALYSIS TO AIRCRAFT DYNAMICS
    WIGDOROWITZ, B
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1992, 15 (03) : 746 - 750
  • [49] Linearization method of nonlinear aeroelastic stability for complete aircraft with high-aspect-ratio wings
    Xie ChangChuan
    Yang Chao
    SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2011, 54 (02) : 403 - 411
  • [50] Linearization method of nonlinear aeroelastic stability for complete aircraft with high-aspect-ratio wings
    XIE ChangChuan * &YANG Chao School of Aerospace Science and Engineering
    Science China Technological Sciences , 2011, (02) : 403 - 411
12345