Integrated sliding mode autopilot-guidance for dual control missiles

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

Volumn 8, Issue , 2005, Pages 6077-6093

  Idan, Moshe ^a,c,d   Shima, Tal ^b,d,e   Golan, Oded M ^b,d,f  

^a TECHNION ISRAEL INSTITUTE OF TECHNOLOGY   (Israel)

^b RAFAEL   (Israel)

^c Faculty of Aerospace Engineering   (Israel)

^d AIAA   (United States)

^e AIR FORCE RESEARCH LABORATORY   (United States)

^f Department 35 ^*  (Israel)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE ALGORITHMS; COMPUTER SIMULATION; CONTROL SYSTEM ANALYSIS; KINEMATICS; MISSILES; NONLINEAR SYSTEMS; REMOTELY OPERATED VEHICLES;

AUTOPILOT-GUIDANCE; DUAL CONTROL MISSILES; TARGET EVASIVE MANEUVERS; ZERO EFFORT MISS (ZEM);

SLIDING MODE CONTROL;

EID: 29744463142     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-6455     Document Type: Conference Paper

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