Stability and Control: Theory, Methods and Applications Ser.
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Cover; Half Title; Title Page; Copyright Page; Contents; Introduction to the Series; Preface; Contributors; 1 Aircraft as Adaptive Nonlinear System which must be in the Adaptational Maximum Zone for Safety; 2 Orbit Determination of a Tethered Satellite System Using Laser and Radar Tracking; 3 Application of Automatic Theorem Proving (ATP) Approach to the Telescope Guidance; 4 Attitude Stability of an Asymmetric Dual-Spin Spacecraft with Stochastic Rotor Speed Fluctuations; 5 Full Envelope Missile Longitudinal Autopilot Design Using the State-Dependent Riccati Equation Method
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14 Building a Parallel Version of a ""Real Gas"" Flow Solver15 A Probabilistic Method to Estimate a Missile Target; 16 Reentry Control for Low UD Vehicles; 17 Exact Euler Aerodynamics via a Novel Method; 18 Singular Penurbations and Time Scales in Aerospace Systems: An Overview; 19 Planning for R & D Manpower in Aviation and Aerospace; 20 Effects of Nonlinearities in Aerodynamic Coefficients on Aircraft Longitudinal Motion; 21 Vector Lyapunov Function Synthesis of Aircraft Control; 22 Control Systems with Parametrical and Structural Reconfiguration; 23 Unified Control Systems
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24 Ergodic Control of Stochastic Navier-Stokes Equation25 Nonlinear Methods and Software for Dynamic Investigations of Fail-Safe Gyromoment Attitude Control Systems of Spacecrafts; Index
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6 Intelligent Control of Agile Aircraft7 Feedback Noise Control in an Acoustic Chamber: Mathematical Theory; 8 Estimation of Asymptotic Stability Regions of Nonlinear Systems by Use of Eigcn-Vectors; 9 Flight Control with and without Control Surfaces: A Nonlinear Look; 10 Optimal Ascent Trajectories for a Single-Stage Suborbital Spacecraft; 11 Nonlinear Dynamics of Two-Body Tethered Satellite Systems; 12 Two and Three-Dimensional Numerical Methods for Free Surface Hydrodynamics; 13 Control of Structures with Self-Straining Actuators: Coupled .Euler/fimoshenko Model: I