Dynamic robust recursive control design and its application to a nonlinear missile autopilot

Proceedings of the American Control Conference

Volumn 1, Issue , 1997, Pages 833-837

  Hull, Richard A ^a   Qu, Zhihua ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ELECTRONIC GUIDANCE SYSTEMS; MATHEMATICAL MODELS; MISSILES; NONLINEAR CONTROL SYSTEMS; ROBUSTNESS (CONTROL SYSTEMS); TIME DOMAIN ANALYSIS;

MISSILE AUTOPILOT;

CONTROL SYSTEM SYNTHESIS;

EID: 0030661150     PISSN: 07431619     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (13)