Multirate LPV synthesis: A loop-shaping approach for missile control

Proceedings of the American Control Conference

Volumn 5, Issue , 2002, Pages 4092-4097

  Farret, D ^a,b   Duc, G ^a   Harcaut, J P ^b  

^a SUPELEC   (France)

^b AIRBUS GROUP INNOVATIONS   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; LINEAR FRACTIONAL TRANSFORMATION; LINEAR PARAMETER VARYING DIGITAL MULTIRATE CONTROLLERS; MISSILE CONTROL;

CONTROL EQUIPMENT; DIGITAL CONTROL SYSTEMS; MATHEMATICAL MODELS; MISSILES; VECTORS;

CONTROL SYSTEM SYNTHESIS;

EID: 0036061019     PISSN: 07431619     EISSN: None     Source Type: Journal    
DOI: 10.1109/ACC.2002.1024570     Document Type: Article

References (13)

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5. A new class of shift-varying operators, their shift-invariant equivalents, and multirate digital systems
6. Dynamic scheduling of modern-robust control autopilot design for missiles
7. Existence conditions of discrete-time strictly proper H controllers
8. Missile autopilot design via a modified LPV synthesis technique
9. Multirate flutter suppression system design for a model wing
10. Robustness analysis of a launcher attitude controller via μ-analysis
11. Self-scheduled H loop-shaping control of a missile