Tailless aircraft control law design using dynamic inversion & μ-synthesis

IEEE Conference on Control Applications - Proceedings

Volumn , Issue , 1996, Pages 107-112

  Ngo, Anhtuan D ^a   Reigelsperger, William C ^a   Banda, Siva S ^a   Bessolo, John A ^a  

^a WRIGHT PATTERSON AIR FORCE BASE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CLOSED LOOP CONTROL SYSTEMS; CONTROL EQUIPMENT; FIGHTER AIRCRAFT; FLIGHT DYNAMICS; MANUAL CONTROL; NONLINEAR EQUATIONS; PERFORMANCE; ROBUSTNESS (CONTROL SYSTEMS); SYSTEM STABILITY; TRACKING (POSITION);

ALL MOVING TIPS; CONTROL EFFECTORS; DIFFERENTIAL LEADING EDGE FLAPS; DYNAMIC INVERSION; FLIGHT CONTROL SYSTEM; LATERAL DIRECTIONAL DYNAMICS; PITCH THRUST VECTORING; SPOILER SLOT DEFLECTOR; TAILLESS AIRCRAFT CONTROL LAW DESIGN; YAW THRUST VECTORING;

CONTROL SYSTEM SYNTHESIS;

EID: 0030368267     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)