Robust control law design for lateral-directional modes of an F-16/MATV using μ-synthesis and dynamic inversion

International Journal of Robust and Nonlinear Control

Volumn 7, Issue 8, 1997, Pages 777-795

  Reigelsperger, William C ^a,b   Hammett, Kelly D ^a,b   Banda, Siva S ^a,c  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b USAF   (United States)

^c Flight Dynamics Directorate   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL SYSTEM ANALYSIS; CONTROL SYSTEM SYNTHESIS; FIGHTER AIRCRAFT; FLIGHT DYNAMICS; MANUAL CONTROL; ROBUSTNESS (CONTROL SYSTEMS); STEP RESPONSE;

DYNAMIC INVERSION; MANUAL FLIGHT CONTROL SYSTEM; ROBUST CONTROL LAW DESIGN;

MOTION CONTROL;

EID: 0031210563     PISSN: 10498923     EISSN: None     Source Type: Journal    
DOI: 10.1002/(SICI)1099-1239(199708)7:8<777::AID-RNC239>3.0.CO;2-D     Document Type: Article

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