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.

About the Author
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.

Reviews
"The text reads very smoothly, and I found it very well edited... I very much enjoyed reading it and find it a welcome addition to the available dynamics and control texts."--American Scientist



Book Information
ISBN 9780691087825
Author Arthur E. Bryson
Format Hardback
Page Count 408
Imprint Princeton University Press
Publisher Princeton University Press
Weight(grams) 482g