Aeroservoelastic structural and control optimization using robust design schemes

Journal of Guidance, Control, and Dynamics

Volumn 25, Issue 1, 2002, Pages 152-159

  Moulin, Boris ^a   Idan, Moshe ^a   Karpel, Mordechay ^a  

^a TECHNION ISRAEL INSTITUTE OF TECHNOLOGY   (Israel)

Author keywords

[No Author keywords available]

Indexed keywords

CONSTRAINT THEORY; ITERATIVE METHODS; MATHEMATICAL MODELS; MATHEMATICAL TRANSFORMATIONS; ROBUSTNESS (CONTROL SYSTEMS); SERVOMECHANISMS; STRUCTURAL OPTIMIZATION;

AEROSERVOELASTIC (ASE) SYSTEMS;

AERODYNAMICS;

EID: 0036152028     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4860     Document Type: Article

References (15)

1. Aeroservoelastic interaction between aircraft structural and control design schemes
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4. Reduced-order models for integrated aeroservoelastic optimization
5. Airplane math modeling methods for active control design
6. Time-domain aeroservoelastic modeling using weighted unsteady aerodynamic forces
7. Control law synthesis and stability robustness improvement using constrained optimization techniques
8. Fictitious mass element in structural dynamics
9. Robust control design strategy with parameter dominated uncertainty
10. Modal-based structural optimization with static aeroelastic and stress constraints
11. Structural optimization with static constraints using extendible modal basis