Effect of sliding mode observers in the homing guidance loop

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering

Volumn 219, Issue 2, 2005, Pages 103-111

  Shkolnikov, I A ^a   Shtessel, Y B ^b,d   Lianos, D P ^c  

^a Intergraph Corporation   (United States)

^b UNIVERSITY OF ALABAMA IN HUNTSVILLE   (United States)

^c US Army Space and Missile Defense Command   (United States)

^d UNIVERSITY OF ALABAMA IN HUNTSVILLE   (United States)

Author keywords

Homing guidance; Sliding mode observers

Indexed keywords

COMPUTER SIMULATION; DYNAMICS; ELECTRONIC GUIDANCE SYSTEMS; FLIGHT DYNAMICS; MATHEMATICAL MODELS; MISSILES; MONTE CARLO METHODS; TARGETS; UNCERTAIN SYSTEMS;

HOMING GUIDANCE; NOISE ATTENUATION; PROPOTIONAL NAVIGATION (PN); SLIDING MODE OBSERVERS;

SLIDING MODE CONTROL;

EID: 21244465971     PISSN: 09544100     EISSN: None     Source Type: Journal    
DOI: 10.1243/095441005X30199     Document Type: Conference Paper

References (10)

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