2026-09-21T14:08:46Z https://www.ideals.illinois.edu/oai-pmh

oai:www.ideals.illinois.edu:2142/16818 2023-07-10 col_2142_5131 col_2142_8888 com_2142_5130 com_2142_8887 com_2142_234

Spong, Mark W. Liu, Yitao 2010-08-20T17:58:46Z 2010-08-20T17:58:46Z 2010-08-20T17:58:46Z 2010-08 This thesis investigates the use of an integrator backstepping controller for a standard helicopter. First, a dynamic model of the helicopter in hovering condition is obtained through the use of Newton-Euler equations. Next, the idea of an integrator backstepping controller is examined followed by the derivation of the actual controller. Finally, simulation results from MATLAB are analyzed and potential future work is proposed. Item withdrawn by Mark Zulauf (zulauf@illinois.edu) on 2010-05-27T13:25:39Z Item was in collections: University of Illinois Theses & Dissertations (ID: 1) No. of bitstreams: 1 Liu_Yitao.pdf: 606265 bytes, checksum: 682f96962b23cda85e55f2d52898aaf7 (MD5) Made available in DSpace on 2010-08-20T17:58:46Z (GMT). No. of bitstreams: 3 Liu_Yitao.pdf: 606265 bytes, checksum: 682f96962b23cda85e55f2d52898aaf7 (MD5) 1_Liu_Yitao.pdf: 606300 bytes, checksum: ea1b6b7b4939be8e3eb9b179b3897647 (MD5) license.txt: 4059 bytes, checksum: c8772c87ffb6a9e0dff7220795dad809 (MD5) http://hdl.handle.net/2142/16818 en Copyright 2010 Yitao Liu integrator backstepping controller standard helicopter model An integrator backstepping controller for a standard helicopter Electrical & Computer Eng 1933 Electrical & Computer Engr 1200 University of Illinois at Urbana-Champaign Thesis M.S. MS:Electr & Computer Eng-UIUC 10KS1200MS