Application of real/mixed μ computational techniques to an H∞ missile autopilot

International Journal of Robust and Nonlinear Control

Volumn 6, Issue 8, 1996, Pages 743-769

  Ferreres, G ^a,b,d   Fromion, V ^a,c   Duc, G ^c   M'Saad, M ^b  

^a Aerospatiale Missiles   (France)

^b GIPSA LAB   (France)

^c SUPELEC   (France)

^d ONERA   (France)

Author keywords

Missile autopilot; Real mixed analysis

Indexed keywords

ALGORITHMS; COMPUTATIONAL COMPLEXITY; COMPUTATIONAL METHODS; CONTROL SYSTEM ANALYSIS; ELECTRONIC GUIDANCE SYSTEMS; MULTIVARIABLE CONTROL SYSTEMS; ROBUSTNESS (CONTROL SYSTEMS);

MIXED COMPUTATIONAL TECHNIQUE; MULTIVARIABLE MISSILE AUTOPILOT; PARAMETRIC AERODYNAMIC UNCERTAINTIES; REAL COMPUTATIONAL TECHNIQUE;

OPTIMAL CONTROL SYSTEMS;

EID: 0030258927     PISSN: 10498923     EISSN: None     Source Type: Journal    
DOI: 10.1002/(sici)1099-1239(199610)6:8<743::aid-rnc187>3.0.co;2-o     Document Type: Article

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