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 -- 6 Intelligent Control of Agile Aircraft -- 7 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 -- 14 Building a Parallel Version of a "Real Gas" Flow Solver -- 15 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 -- 24 Ergodic Control of Stochastic Navier-Stokes Equation.
Text of Note
25 Nonlinear Methods and Software for Dynamic Investigations of Fail-Safe Gyromoment Attitude Control Systems of Spacecrafts -- Index.