Control of Spacecraft and Aircraft
Princeton University Press (Verlag)
978-0-691-08782-5 (ISBN)
Here a leading researcher provides a comprehensive treatment of the design of automatic control logic for spacecraft and aircraft. In this book Arthur Bryson describes the linear-quadratic-regulator (LQR) method of feedback control synthesis, which coordinates multiple controls, producing graceful maneuvers comparable to those of an expert pilot. The first half of the work is about attitude control of rigid and flexible spacecraft using momentum wheels, spin, fixed thrusters, and gimbaled engines. Guidance for nearly circular orbits is discussed. The second half is about aircraft attitude and flight path control. This section discusses autopilot designs for cruise, climb-descent, coordinated turns, and automatic landing. One chapter deals with controlling helicopters near hover, and another offers an introduction to the stabilization of aeroelastic instabilities. Throughout the book there is a strong emphasis on the mathematical modeling necessary for designing a good feedback control system. The appendixes summarize analysis of linear dynamic systems, synthesis of analog and digital feedback control, simulation, and modeling of flexible vehicles.
Arthur E. Bryson, Jr., is Paul Pigott Professor of Engineering at Stanford University. Coauthor, with Y. C. Ho, of Applied Optimal Control (Blaisdell/ Hemisphere), he is a member of the National Academy of Engineering and the National Academy of Sciences.
List of FiguresList of TablesPreface and AcknowledgmentsCh. 1Natural Motions of Rigid Spacecraft1Ch. 2Spacecraft Sensors and Attitude Determination16Ch. 3Attitude Control with Thrusters28Ch. 4Attitude Control with Reaction Wheels37Ch. 5Attitude Stabilization with Spin50Ch. 6Attitude Control with a Gimbaled Momentum Wheel74Ch. 7Attitude Control during Thrust Maneuvers93Ch. 8Control of Translational Motions102Ch. 9Flexibility and Fuel Slosh114Ch. 10Natural Motions of Rigid Aircraft142Ch. 11Aircraft Sensors164Ch. 12Control of Longitudinal Motions of Aircraft179Ch. 13Control of Lateral Motions of Aircraft232Ch. 14Control of Helicopters near Hover271Ch. 15Aeroelastic Systems284Appendix A - Linear System Representations301Appendix B - Steady-State Control311Appendix C - Synthesis of Analog Control Logic317Appendix D - Synthesis of Digital Control Logic328Appendix E - Simulation343Appendix F - Modeling Flexible Systems350References369Index377
| Erscheint lt. Verlag | 5.6.1994 |
|---|---|
| Verlagsort | New Jersey |
| Sprache | englisch |
| Maße | 152 x 235 mm |
| Gewicht | 482 g |
| Themenwelt | Technik ► Elektrotechnik / Energietechnik |
| Technik ► Fahrzeugbau / Schiffbau | |
| Technik ► Luft- / Raumfahrttechnik | |
| ISBN-10 | 0-691-08782-2 / 0691087822 |
| ISBN-13 | 978-0-691-08782-5 / 9780691087825 |
| Zustand | Neuware |
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