Guidance and autopilot for missiles steered by aerodynamic lift and divert thrusters using second order sliding modes

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference 2006

Volumn 8, Issue , 2006, Pages 5250-5271

  Shtessel, Yuri ^a,d,e   Tournes, Christian ^a,b,d,e   Shkolnikov, Ilya ^c  

^a UNIVERSITY OF ALABAMA IN HUNTSVILLE   (United States)

^b Davidson Technologies Inc   (United States)

^c Z/I Imaging Corporation   (United States)

^d AIAA   (United States)

^e IEEE

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LIFTS; ATTITUDE THRUSTERS; AUTOPILOT STEERING; DIVERT THRUSTERS;

AERODYNAMICS; COMPUTER SIMULATION; MANEUVERABILITY; MISSILES; ROBUSTNESS (CONTROL SYSTEMS); SLIDING MODE CONTROL;

ELECTRONIC GUIDANCE SYSTEMS;

EID: 33845736911     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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