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- Category: A PRACTICAL. APPROACH TO. ROBUSTNESS. ANALYSIS
- Conclusion
- AN APPLICATION
- A SKEWED ц PROBLEM
- EXTENSION TO THE CASE OF PARAMETRIC UNCERTAINTIES
- A SECOND ц BASED METHOD
- THE USE OF д BOUNDS
- AN EXTENSION
- A GENERALIZED CONDITION OF OSCILLATION
- . A PRELIMINARY TECHNICAL RESULT
- A FIRST /X BASED METHOD
- AN EXTENSION
- 2. A GRAPHICAL METHOD
- NONLINEAR ANALYSIS IN THE PRESENCE OF PARAMETRIC UNCERTAINTIES
- APPLICATION TO THE MISSILE
- AN IMPROVED ALGORITHM
- COMPUTATIONAL METHOD
- INTRODUCTION OF MODEL UNCERTAINTIES
- A STRUCTURED APPROACH
- AN UNSTRUCTURED APPROACH
- AN ALTERNATIVE SMALL GAIN APPROACH
- THE DETAILED METHOD
- DETAILED ALGORITHM
- COMPUTATION OF THE ROBUST DELAY MARGIN
- A GENERIC EXAMPLE
- ROBUSTNESS ANALYSIS IN THE PRESENCE OF TIME DELAYS
- THE TELESCOPE MOCK-UP
- COMPUTATION AROUND THE CRITICAL FREQUENCY
- COMPUTATION OF A LOWER BOUND OF Umax
- APPLICATION OF THE IMPROVED ALGORITHM
- APPLICATION OF THE BASIC ALGORITHM
- APPLICATION TO THE FLEXIBLE AIRCRAFT
- AN IMPROVEMENT
- AN ALGORITHM THE BASIC ALGORITHM
- CHECKING THE VALIDITY OF D, G SCALING MATRICES
- . INTRODUCTION OF THE FREQUENCY
- CHECKING A POSTERIORI THE VALIDITY OF D, G SCALING MATRICES ON A FREQUENCY INTERVAL
- A THEORETICAL JUSTIFICATION OF THE APPROACH
- COMPUTATION OF D, G SCALING
- 2. RELATIONSHIP BETWEEN BOTH FORMULATIONS OF THE ц UPPER BOUND
- ROBUSTNESS ANALYSIS OF FLEXIBLE STRUCTURES
- 4. A FURTHER STUDY OF THE и UPPER BOUNDS
- ROBUST PERFORMANCE
- ROBUST STABILITY
- APPLICATION OF THE SKEWED д TOOLS
- SUMMARY
- A SKEWED Ц LOWER BOUND
- COMPUTATION OF SCALING MATRICES £>! AND Gx
- AN AUGMENTED p PROBLEM
- THE CASE OF STRUCTURED UNCERTAINTIES
- A SECOND і/ UPPER BOUND
- COMPUTATION OF SKEWED i BOUNDS
- GAIN-SCHEDULED AND ADAPTIVE ROBUST CONTROL
- PARAMETRIC ROBUSTNESS ANALYSIS
- DIRECT COMPUTATION OF THE MAXIMAL S. S. V
- . NONLINEAR ANALYSIS IN THE FACE OF PARAMETRIC UNCERTAINTIES
- CHECKING A SMALL GAIN CONDITION DESPITE MODEL UNCERTAINTIES
- SKEWED /х PROBLEMS IN ROBUSTNESS ANALYSIS
- AN ADDITIONAL COMPARISON
- ROBUST PERFORMANCE (P5)
- THE TRANSPORT AIRCRAFT
- CONCLUSION
- ROBUST PERFORMANCE: SENSITIVITY FUNCTION (P3)
- ROBUST PERFORMANCE: POLE LOCATION (P2)
- ROBUST STABILITY (P1)
- APPLICATIONS OF THE /x TOOLS
- MIGRATION OF THE CLOSED LOOP POLES THROUGH THE IMAGINARY AXIS: AN LP METHOD
- MIGRATION OF THE CLOSED LOOP POLES THROUGH THE IMAGINARY AXIS: A FIRST SIMPLE METHOD
- REGULARIZATION OF THE PROBLEM
- A REAL ^ LOWER BOUND
- A MIXED Ц LOWER BOUND
- A SECOND MIXED і UPPER BOUND
- A FIRST MIXED д UPPER BOUND
- A COMPLEX ^ UPPER BOUND
- COMPUTATION OF THE MIXED S. S. V
- JONES’ METHOD
- DAILEY’S METHOD
- COMPUTATION OF i BOUNDS
- THE FLEXIBLE LFT MODEL
- AN ALTERNATIVE METHOD FOR INTRODUCING UNCERTAINTIES IN THE FLEXIBLE MODEL
- THE TRANSPORT AIRCRAFT
- MORTON’S METHOD
- APPLICATIONS
- SIMPLE METHOD FOR PHYSICAL MODELS
- CHENG AND DE MOOR’S METHOD
- THE GENERAL CASE
- AFFINE UNCERTAINTIES
- REALIZATION OF UNCERTAIN SYSTEMS UNDER AN LFT FORM
- . THE TELESCOPE MOCK-UP
- APPLICATION
- DESIGN OF THE Нж AUTOPILOT
- THE LINEARIZED MODEL
- THE NONLINEAR MODEL
- A MISSILE PROBLEM
- DESIGN OF A FLEXIBLE CONTROLLER
- . THE FLEXIBLE MODEL
- . DESIGN OF A RIGID CONTROL LAW
- THE AERODYNAMIC MODEL
- APPLICATIVE EXAMPLES
- THE SPECIAL CASE OF FLEXIBLE SYSTEMS