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E-raamat: Nonlinear Problems in Aviation and Aerospace [Taylor & Francis e-raamat]

Edited by (Embry-Riddle Aeronautical University, Florida, USA)
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The study of nonlinear phenomena in aviation and aerospace includes developments in computer technology and the use of nonlinear mathematical models. Nonlinearities are a feature of aircraft dynamics and flight control systems and need to respond to achieve stability and performance. This multiauthor volume comprises selected papers from the conference Nonlinear Problems in Aviation and Aerospace at Embry-Riddle Aeronautical University and additional invited papers from many distinguished scientists. Coverage includes orbit determination of a tethered satellite system using laser and radar tracking, and intelligent control of agile aircraft, flight control with and without control surfaces.
Introduction to the Series xi Preface xiii Contributors xv Aircraft as Adaptive Nonlinear System which must be in the Adaptational Maximum Zone for Safety 1(10) M. Ignatiev S. Sivasundaram N. Simatos Orbit Determination of a Tethered Satellite System Using Laser and Radar Tracking 11(14) S.R. Vadali H. Jung K.T. Alfriend Application of Automatic Theorem Proving (ATP) Approach to the Telescope Guidance 25(18) E. Cherkashin S. Vassilyev Attitude Stability of an Asymmetric Dual-Spin Spacecraft with Stochastic Rotor Speed Fluctuations 43(14) S.F. Asokanthan X.-H. Wang Full Envelope Missile Longitudinal Autopilot Design Using the State-Dependent Riccati Equation Method 57(20) C.P. Mracek J.R. Cloutier Intelligent Control of Agile Aricraft 77(12) R.R. Mohler R.R. Zakrzewski Feedback Noise Control in an Acoustic Chamber: Mathematical Theory 89(24) I. Lasiecka R. Triggiani Estimation of Asymptotic Stability Regions of Nonlinear Systems by Use of Eigen-Vectors 113(10) H-K. Lee K-W. Han Flight Control with and without Control Surfaces: A Nonlinear Look 123(16) L. Tian P. Lu J.J. Burken Optimal Ascent Trajectories for a Single-Stage Suborbital Spacecraft 139(14) A. Miele S. Mancuso Nonlinear Dynamics of Two-Body Tethered Satellite Systems 153(14) A.K. Misra M.S. Nixon V.J. Modi Two and Three-Dimensional Numerical Methods for Free Surface Hydrodynamics 167(12) V. Casulli P. Zanolli Control of Structures with Self-Straining Actuators: Coupled Euler/Timoshenko Model: I 179(16) A.V. Balakrishnan Building a Parallel Version of a ``Real Gas Flow Solver 195(14) R.L. Carino C.F. Cox J. Zhu P. Cinnella A Probabilistic Method to Estimate a Missile Target 209(12) E. Duflos P. Vanheeghe P. Penel P. Borne Reentry Control for Low L/D Vehicles 221(16) A. Cavallo G. De Maria Exact Euler Aerodynamics via a Novel Method 237(14) F.R. Payne Singular Perturbations and Time Scales in Aerospace Systems: An Overview 251(14) D. S. Naidu Planning for R&D Manpower in Aviation and Aerospace 265(16) G. Leitmann C.S. Lee Effects of Nonlinearities in Aerodynamic Coefficients on Aircraft Longitudinal Motion 281(16) J. Rohacs P. Granasy Vector Lyapunov Function Synthesis of Aircraft Control 297(20) L.T. Gruyitch Control Systems with Parametrical and Structural Reconfiguration 317(12) S.A. Doganovsky N.N. Maksimkin S. Sivasundaram S. Sliwa S.N. Vassilyev Unified Control Systems 329(20) S. Sivasundaram Ergodic Control of Stochastic Navier-Stokes Equation 349(10) S.S. Sritharan P. Sundar Nonlinear Methods and Software for Dynamic Investigations of Fail-Safe Gyromoment Attitude Control Systems of Spacecrafts 359(16) V.M. Matrosov M.F. Reshetnev V.A. Rayevsky Y.I. Somov Index 375
S. Sivasundaram