Optimal design of integrated missile guidance and control

AIAA and SAE World Aviation Conference, 1998

Volumn , Issue , 1998, Pages

  Lin, Ching Fang ^a   Ohlmeyer, Ernest ^b   Bibel, John E ^b   Malyevac, Steve ^b  

^a AMERICAN GNC CORPORATION   (United States)

^b NAVAL SURFACE WARFARE CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIR NAVIGATION; BALLISTIC MISSILES; BALLISTICS; BLENDING; COMPUTER CIRCUITS; EARTH ATMOSPHERE; ELECTRONIC GUIDANCE SYSTEMS; FUZZY LOGIC; MISSILES; RECONFIGURABLE HARDWARE;

AERODYNAMIC SURFACES; DYNAMICS AND CONTROL; GUIDANCE AND CONTROL LAWS; INNOVATIVE APPROACHES; INTEGRATED GUIDANCE AND CONTROLS; RESPONSE CHARACTERISTIC; SKID-TO-TURN MISSILES; TACTICAL BALLISTIC MISSILES;

GUIDED MISSILES;

EID: 84976629792     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (13)

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