دینامیک و کنترل وسایل فضایی (کودکان به جلو)

"Space Vehicle Dynamics and Control" provides a solid foundation in mathematics modelling analysis and control of space vehicles. More than 200 figures, photographs and tables are featured in detailed sections covering the fundamentals of orbital, attitude and structural motions of space vehicles. The textbook highlights a range of orbital manoeuvring issues: orbital transfer, rendezvous, orbit control and halo orbit determination. Rotational manoeuvre and attitude control of rigid spacecraft under the influence of reaction jet firings, internal energy dissipation and robotic manipulators in the presence of structural modelling uncertainties are also discussed. At the end of each chapter, Dr. Wie includes a helpful list of references for graduate students and working professionals studying spacecraft design. "Space Vehicle Dynamics and Control" requires a thorough knowledge of vector and matrix algebra, calculus, ordinary differential equations, linear system dynamics and engineering mechanics. Some familiarity with structural dynamics and partial differential equations is presumed, and because some problems may require the use of software for the analysis control design and numerical simulation, readers should have access to computational software (ie MATLAB) on a personal computer. Front Matter......Page 1 Foreword......Page 3 Preface......Page 4 Table of Contents......Page 0 Front Matter......Page 7 Foreword......Page 9 Preface......Page 10 Table of Contents......Page 13 4......Page 16 1.1 Matrix and Vector Analysis......Page 17 1.2 Classical Mechanics......Page 34 1.3 Dynamic Systems Analysis......Page 82 2.1 Feedback Control Systems......Page 128 2.2 Classical Frequency-Domain Methods......Page 130 2.3 Classical Gain-Phase Stabilization......Page 142 2.4 Digital Control......Page 158 2.5 Modern State-Space Methods......Page 166 2.6 Stability Robustness Analysis......Page 189 2.7 Robust Control of Uncertain Dynamic Systems......Page 208 6......Page 220 3.1 Two-Body Problem......Page 221 3.2 Geometry of Conic Sections......Page 228 3.3 Vis-Viva Equation......Page 232 3.4 Kepler's Time Equation......Page 234 3.5 Orbital Position and Velocity......Page 237 3.6 Orbital Perturbations......Page 245 3.7 Circular Restricted Three-Body Problem......Page 252 3.8 Elliptic Restricted Three-Body Problem......Page 268 4.1 Launch Vehicle Trajectories......Page 273 4.2 Orbit Injection......Page 279 4.3 Single-Impulse Maneuvers......Page 282 4.4 Hohmann Transfer......Page 283 4.5 Interplanetary Flight......Page 286 4.6 Orbital Rendezvous......Page 294 4.7 Halo Orbit Determination and Control......Page 298 8......Page 316 5.1 Direction Cosine Matrix......Page 317 5.2 Euler Angles......Page 320 5.3 Euler's Eigenaxis Rotation......Page 322 5.4 Quaternions......Page 328 5.5 Kinematic Differential Equations......Page 332 6.1 Angular Momentum of a Rigid Body......Page 340 6.2 Inertia Matrix and Inertia Dyadic......Page 341 6.3 Principal Axes......Page 346 6.4 Euler's Rotational Equations of Motion......Page 349 6.5 Torque-Free Motion of an Axisymmetric Rigid Body......Page 352 6.6 General Torque-Free Motion......Page 356 6.7 Stability of Torque-Free Motion About Principal Axes......Page 359 6.8 Spinning Axisymmetric Body with Constant Body-Fixed Torque......Page 361 6.9 Asymmetric Rigid Body with Constant Body-Fixed Torques......Page 364 6.10 Rigid Body in a Circular Orbit......Page 374 6.11 Gyrostat in a Circular Orbit......Page 383 6.12 Dual-Spinner with a Platform Damper......Page 385 7.1 Control of Spinning Spacecraft......Page 390 7.2 Time-Optimal Reorientation Maneuvers......Page 401 7.3 Quaternion-Feedback Reorientation Maneuvers......Page 411 7.4 Attitude Control and Momentum Management......Page 428 7.5 Steering Logic for Control Moment Gyros......Page 444 7.6 Optimal Jet Selection Logic......Page 454 7.7 Pulse-Modulated Attitude Control......Page 460 11......Page 469 8.2 Uniform Bars......Page 470 8.3 Uniform Beams......Page 479 8.4 Rigid Body with Beamlike Appendages......Page 488 8.5 Rigid/Flexible Frame with a Pretensioned Membrane......Page 492 8.6 Flexible Toroidal Structures......Page 498 8.7 Summary......Page 508 9.1 Thrust Vector Control Design for a Spacecraft with Propellant Sloshing......Page 510 9.2 Attitude Control Design for a Bias-Momentum Stabilized Spacecraft......Page 521 9.3 Stationkeeping Attitude Control of a Flexible Spacecraft......Page 533 9.4 Nonlinear Pulse-Modulated Control Analysis and Design......Page 541 9.5 Attitude Control Redesign for the Hubble Space Telescope......Page 554 9.6 Active Structural Vibration Control......Page 564 9.7 Summary......Page 587 10.1 Time-Optimal Control......Page 591 10.2 Robust Time-Optimal Control......Page 601 10.3 Robust Time-Optimal Control Using One-Sided Control Inputs......Page 608 10.4 Robust Fuel- and Time-Optimal Control......Page 613 10.5 Robustified Feedforward and Feedback Control......Page 629 Bibliography......Page 640 C......Page 658 E......Page 659 H......Page 660 L......Page 661 M......Page 662 P......Page 663 R......Page 664 S......Page 665 Z......Page 666 Space Vehicle Dynamics and Control provides a solid foundation in dynamic modeling, analysis, and control of space vehicles. More than 200 figures, photographs, and tables are featured in detailed sections covering the fundamentals of controlling orbital, attitude, and structural motions of space vehicles. The textbook highlights a range of orbital maneuvering and control problems : orbital transfer, rendezvous, and halo orbit determination and control. Rotational maneuvering and attitude control problems of space vehicles under the influence of reaction jet firings, internal energy dissipation, or momentum transfer via reaction wheels and control moment gyros are treated in detail. The textbook also highlights the analysis and design of attitude control systems in the presence of structural flexibility and/or propellant sloshing. At the end of each chapter, Dr. Wie includes a helpful list of references for graduate students and working professionals studying spacecraft dynamics and control. A bibliography of more than 350 additional references in the field of spacecraft guidance, control, and dynamics is also provided at the end of the book. Space vehicle dynamics and control requires a thorough knowledge of vector and matrix algebra, calculus, ordinary differential equations, engineering mechanics, and linear system dynamics and control. The first two chapters provide a summary of such necessary background material. Since some problems may require the use of software for the analysis, control design, and numerical simulation, readers should have access to computational software (i.e., MATLAB) on a personal computer