Missile autopilot designs using H∞ control with gain scheduling and dynamic inversion

Journal of Guidance, Control, and Dynamics

Volumn 21, Issue 2, 1998, Pages 234-243

  Schumacher, Corey ^a,b,c   Khargonekar, Pramod P ^a,b  

^a UNIVERSITY OF MICHIGAN   (United States)

^b Department of Aerospace Engineering ^*  (United States)

^c AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; ELECTRONIC GUIDANCE SYSTEMS; FREQUENCY DOMAIN ANALYSIS; LINEARIZATION; NONLINEAR CONTROL SYSTEMS; ROBUSTNESS (CONTROL SYSTEMS); TIME DOMAIN ANALYSIS;

DYNAMIC INVERSION CONTROL SYSTEMS; GAIN SCHEDULING;

AUTOMATIC PILOTS;

EID: 0032027993     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4248     Document Type: Article

References (17)

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