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ICNPAA 2002 International Conference on Nonlinear Problems in Aviation and Aerospace
May 15-17, 2002
Florida Institute of Technology
Melbourne, FL, USA

Organizers
S. Sivasundaram

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Abstracts

This is an archive of abstracts accepted to this conference. For more listing and sorting options, see the active list.

A. V. Balakrishnan On The (Non-Numeric) Mathematical Foundations of Aeroelasticity
Silviu Birauas Closed orbits of the Boussinesq system in a time dependent cylindrical domain
Liliana Braescu The effect of the meniscus weight on the diameter control of the silicon filament, grown from the melt in a vacuum by E.F.G. method
Arthur G. Cave Nonlinear Stability and Optimization Techniques
Joon Chung Chaos and Nonlinear Heave Dynamics of an Air Cushion Vehicle Bag and Finger Skirt
Bill Clark Optimizing the Earth to Mars Trajectory
John T. Conway Application of an Exact Nonlinear Actuator Disk Theory to Wind Turbines
Waldemar de Castro Leite Filho Discrete-time adaptive control for continuous-time system
Denny Fritze A concept for the modification of the geometry of a curved shell structure for minimizing radiated sound power
G. Gui Selection of Nozzle Location in Pressure Die Casting
Wassim M. Haddad A Unified Framework for Analysis and Synthesis of Hybrid Dynamical Systems
Harry H. Hilton Viscoelastic column dynamic creep buckling - failure probabilities and survival times
Fumiaki Imado Some Approaches to Optimal Pursuit Evasion Air Combat Games
Victoria Iordan The control of a vehicle motion lengthways a branch of asymptotically stable steady-states
Kazuhisa Ito Nonlinear Robust Output Tracking with Almost Disturbance Decoupling
Eva Kaslik The control of a vehicle motion lengthways a path of unstable steady-states
Qihong Ke New phase plane for determining limit cycles and stability of digital systems
Valery A. Kholodnyi Universal Contingent Claims and Multiplicative Measures: Examples and Applications
Artur Korgul Method of lossless differentiating and numerical solving of nonlinear inverse problems
G. S. Ladde A Few Recent Advances in the Study of Hybrid Systems
Yuri S. Ledyaev Robust discontinuous feedback in optimal control and stabilization
Raja Loganantharaj Towards Solving Hard Problems: Achievements in the past, Current works and the Future Challenges
Wolfgang G. Luber Nonlinear Flutter Prediction of a Combat Aircraft Involving Backlash and Actuator Failures on Control Surfaces
Silvanus Owuoth Magundho Solution of Elastic contact problems
Steffen Marburg Aspects of Structural-Acoustic Modeling and Optimization
Monica Mihailovici On the crystallographic quality improvement of a semiconductor crystal grown in a low gravity environment by Bridgman-Stockbarger method
Hiroyuki Miyamoto Design of Nonlinear Plug-In Adaptive Control Systems
Adrian Neculae On the gravity effect on the mass transport in a hydrothermal system
Sigeru Omatu Neuro-PID Control for Stabilization of Inverted Pendulums
Vladislav Rutkovsky An approach to designing of an adaptive system of the gearbox clearance tuning of gas turbine engines flexible shaft rotor
Alaa Shawky Modeling and Nonlinear Predictive Control of Flexible Manipulator
Dongho Shin Design of Neural Network Adaptive Control Law for Aircraft System including Uncertainty
Krzysztof Sibilski Analysis of the Behaviour of a Vectored Thrust Aircraft at High Angles of Attack by Continuation and Bifurcation Methods
Lijie Su An Isometric Surface Method for Integer Linear Programming
Ozan Tekinalp On the Guidance and Control of a Spinning Missile
Eugenia Tulcan-Paulescu Thermotransport and initial conditions in the axial and radial macrosegregation during directional solidification
S. Vassilyev Necessary and sufficient conditions for accessibility of automata networks
Aghalaya S. Vatsala Practical Stability of Hybrid Impulsive Systems
R. Visser Source Identification in Structural Acoustics with an Inverse Frequency Response Function Technique
Daoyi Xu A New Approach to Exponential Stability Analysis for Hopfield Neural Networks with delays
Woosoon Yim Nonlinear Control of a Prototypical Aeroelastic Wing Section: State-Dependent Riccati Equation Method


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