Sliding Mode Integrated missile Guidance and Control

AIAA Guidance, Navigation, and Control Conference

Volumn , Issue , 2010, Pages

  Harl, Nathan ^a   Balakrishnan, S N ^a   Phillips, Craig ^b  

^a IST Rolla   (United States)

^b NAVAL SURFACE WARFARE CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC EFFECT; CONTROL ARCHITECTURE; DESIGN PROCESS; FINITE TIME; GUIDANCE AND CONTROL; GUIDANCE AND CONTROL SYSTEM; HEADING ERROR; HIT-TO-KILL; IMPACT POINT; INTEGRATED GUIDANCE; MANEUVERING TARGETS; MISS DISTANCE; NON-LINEAR MISSILE; NUMERICAL RESULTS; SINGLE LOOP; SLIDING MODE TECHNIQUES; SLIDING MODES; TARGET ACCELERATION;

COMPUTER SIMULATION; MISSILES; UNCERTAINTY ANALYSIS;

ELECTRONIC GUIDANCE SYSTEMS;

EID: 84867775584     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2010-7741     Document Type: Conference Paper

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