Stabilization of a mini rotorcraft with four rotors

被引:238
作者
Castillo, P
Lozano, R
Dzul, A
机构
[1] CNRS, UMR 6599, Heudiasyc UTC, F-60205 Compiegne, France
[2] CNRS, Lab Heudiasyc Heurist Diagnost Syst Complexes, F-60205 Compiegne, France
[3] Inst Tecnol La Laguna, Dept Elect & Elect Engn, San Cristobal la Laguna, Spain
来源
IEEE CONTROL SYSTEMS MAGAZINE | 2005年 / 25卷 / 06期
关键词
D O I
10.1109/MCS.2005.1550152
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
[No abstract available]
引用
收藏
页码:45 / 55
页数:11
相关论文
共 13 条
  • [1] Alderete T. S., SIMULATOR AERO MODEL
  • [2] Castillo P., 2005, ADV IND CON
  • [3] Etkin B., 1959, Dynamics of Flight, V3rd ed.
  • [4] FANTONI I, 2001, CONTROL NONLINEAR ME
  • [5] GAVRILETS V, 2002, P AIAA MONT CA AUG, P4834
  • [6] Goldstein H, 1980, CLASSICAL MECH
  • [7] NONLINEAR CONTROL DESIGN FOR SLIGHTLY NONMINIMUM PHASE SYSTEMS - APPLICATION TO V/STOL AIRCRAFT
    HAUSER, J
    SASTRY, S
    MEYER, G
    [J]. AUTOMATICA, 1992, 28 (04) : 665 - 679
  • [8] Autonomous vertical landing on an oscillating platform: an internal-model based approach
    Marconi, L
    Isidori, A
    Serrani, A
    [J]. AUTOMATICA, 2002, 38 (01) : 21 - 32
  • [9] MCCORMICK BW, 1995, AERODYNMICS AERONAUT
  • [10] SACCO N, 2002, ROTORY MAG