Integrated guidance and autopilot design for a chasing UAV via high-order sliding modes

Journal of the Franklin Institute

Volumn 349, Issue 2, 2012, Pages 531-558

  Yamasaki, Takeshi ^a   Balakrishnan, S N ^b   Takano, Hiroyuki ^a  

^a NATIONAL DEFENSE ACADEMY   (Japan)

^b University of Missouri Rolla   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT APPLICATIONS; AUTOPILOT DESIGNS; AUTOPILOT SCHEME; CONTROL VARIABLE; DESIGN SYNTHESIS; GUIDANCE AND CONTROL; GUIDANCE LAWS; HIGH ORDER SLIDING MODE; INTEGRATED GUIDANCE; PARTIAL DERIVATIVES; SECOND ORDER SLIDING MODES; SECOND ORDERS; SIMULATION PERFORMANCE; SLIDING STRUCTURE; SLIDING SURFACE; TUNING PARAMETER; UNINHABITED AERIAL VEHICLE;

AIRCRAFT CONTROL; DESIGN; INTEGRATION; SURFACE STRUCTURE;

SLIDING MODE CONTROL;

EID: 84856490133     PISSN: 00160032     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.jfranklin.2011.08.004     Document Type: Article

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