Autopilot design for a missile with reaction-jet using coefficient diagram method

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2001, Pages

  Hirokawa, Rui ^a   Sato, Koichi ^a   Manabe, Shunji ^b  

^a MITSUBISHI ELECTRIC CORPORATION   (Japan)

^b Department of Defense Engineering ^*  (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

AIR NAVIGATION; DESIGN; ECONOMIC AND SOCIAL EFFECTS; FEEDBACK CONTROL; FEEDFORWARD CONTROL; FINS (HEAT EXCHANGE); MISSILES; VERTICAL STABILIZERS;

COEFFICIENT DIAGRAM METHOD; CONVENTIONAL DESIGN; FEED-FORWARD CONTROLLERS; FEEDBACK CONTROLLER; GUIDANCE PERFORMANCE; MANEUVERABLE TARGETS; MINIMUM FUEL CONSUMPTION; MULTIPLE INPUTS AND MULTIPLE OUTPUTS;

CONTROLLERS;

EID: 85087593877     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-4162     Document Type: Conference Paper

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