A sliding mode missile pitch autopilot synthesis for high angle of attack maneuvering

IEEE Transactions on Control Systems Technology

Volumn 6, Issue 3, 1998, Pages 359-371

  Thukral, Ajay ^b   Innocenti, Mario ^a,c  

^a IEEE

^b TUSKEGEE UNIVERSITY   (United States)

^c UNIVERSITY OF PISA   (Italy)

Author keywords

Control systems; Missile control; Robustness; Scheduling; Variable structure systems

Indexed keywords

AERODYNAMICS; AUTOMATIC PILOTS; CONTROL SYSTEM SYNTHESIS; CONTROLLABILITY; MISSILES; ROBUSTNESS (CONTROL SYSTEMS);

ANGLE OF ATTACK; FLIGHT ENVELOPE; MISSILE CONTROL;

ELECTRONIC GUIDANCE SYSTEMS;

EID: 0032071047     PISSN: 10636536     EISSN: None     Source Type: Journal    
DOI: 10.1109/87.668037     Document Type: Article

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