Advances in dynamics and control

S. Sivasundaram

334 pages, parution le 25/05/2004

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Résumé

Nonlinear phenomena encountered in aviation and aerospace applications have stimulated cooperation among engineers and scientists from a range of disciplines. Developments in computer technology now allow solutions to many nonlinear problems, and industrial recognition of the use and applications of nonlinear mathematical models for solving technological problems is on the rise.

Advances in Dynamics and Control clearly reflects the effectiveness of this interdisciplinary cooperation. This carefully edited volume contains research papers contributed by international experts that explore many new ideas, results, and research directions. These papers cover a wide range of topics, including rotorcraft dynamics, stabilization of unstable aircraft, spacecraft and satellite dynamics and control, missile auto-pilot and guidance design, hybrid system dynamics and control, intelligent control, neuro-fuzzy techniques, and structural and acoustic modeling.

Features

Explores new ideas, reviews the latest results, and discusses emerging directions in aerospace and aviation applications of dynamics and control.
Presents research papers contributed by an international, interdisciplinary panel of experts.
Provides a valuable source of reference for students in applied mathematics, space physics and aerospace engineering, mechanical engineering, and electrical engineering, and for researchers working in nonlinear dynamics and control

Sommaire

Global Spacecraft Attitude Control Using Magnetic Actuators
Adaptive Learning Control for Spacecraft Formation Flying
Spectral Properties of the Generalized Resolvent Operator for an Aircraft Wing Model in Subsonic
Bifurcation Analysis for the Inertial Coupling Problem of a Reentry Vehicle
Missile Autopilot Design Using Dynamic Fuzzy Gain-Scheduling Technique
Model Predictive Control of Nonlinear Rotorcraft Dynamics with Application to the XV-15 Tilt Rotor
New Development of Vector Lyapunov Functions and Airplane Control Synthesis
Stabilization of Unstable Aircraft Dynamics under Control Constraints
QUEST Algorithms Case Study: GPS-Based Attitude Determination of Gyrostat Satellite
Asymptotic Controllability in Terms of Two Measures of Hybrid Dynamic Systems
Exact Boundary Controllability of a Hybrid PDE System Arising in Structural Acoustic Modeling
Flow Field, Temperature, and Dopant Concentration Evolution in a Bridgman-Stockbarger Crystal
Growth System in a Strictly Zero-Gravity and a Low-Gravity Environment
Identification of Stiffness Matrices of Structural and Mechanical Systems from Modal Data
A Survey of Applications in Structural-Acoustic Optimization for Passive Noise Control with a Focus on Optimal Shell Contour
Intelligent Control of Aircraft Dynamic Systems with a New Hybrid Neuro-Fuzzy-Fractal Approach
Closed-Form Solution of Three-Dimensional Ideal Proportional Navigation
Guidance Design with Nonlinear Control
ISA Control Algorithm for Nonlinear Multiconnected Objects
Optimal Control and Differential Riccati Equations under Singular Estimates for eMB in the Absence of Analyticity
Nonlinear Problems of Spacecraft Fault-Tolerant Control Systems

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Caractéristiques techniques

	PAPIER
Éditeur(s)	Chapman and Hall / CRC
Auteur(s)	S. Sivasundaram
Parution	25/05/2004
Nb. de pages	334
Format	16 x 24
Couverture	Relié
Poids	606g
Intérieur	Noir et Blanc
EAN13	9780415308526
ISBN13	978-0-415-30852-6