Effects of Structural Flexibility on Launch Vehicle Control Systems
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 60 |
Release | : 1970 |
Genre | : Space vehicles |
ISBN | : |
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Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 60 |
Release | : 1970 |
Genre | : Space vehicles |
ISBN | : |
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 80 |
Release | : 1972 |
Genre | : Space vehicles |
ISBN | : |
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 52 |
Release | : 1969 |
Genre | : Space vehicles |
ISBN | : |
Author | : National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : |
Release | : 1969 |
Genre | : |
ISBN | : |
Author | : United States. National Aeronautics and Space Administration. Space Vehicle Design Criteria (Guidance and Control) |
Publisher | : |
Total Pages | : 62 |
Release | : 1972 |
Genre | : Space vehicles |
ISBN | : |
Author | : W. A. Wagner |
Publisher | : |
Total Pages | : 172 |
Release | : 1974 |
Genre | : Liquid propellant rockets |
ISBN | : |
Author | : Chong Hun Kim |
Publisher | : Lulu.com |
Total Pages | : 676 |
Release | : 2007 |
Genre | : Technology & Engineering |
ISBN | : 0615165117 |
This book is written for aerospace engineers who have completed their BS degree and are interested in the design and analysis of rocket attitude control systems. It introduces a new approach to the design, characterized by its robustness. Current LV attitude control systems are designed based on classical SISO control theory, and they lack robustness. The theory used here truly offers a technique that enables us to design control systems that are reasonably insensitive to math modeling errors and can withstand disturbances such as gust, and in addition it doesn’t need external states estimator, such as Kalman filtering. Extensive simulation results, which demonstrate the effectiveness of this approach, are presented in this book. Basic rocket theory and a concept of H-infinity control system design technique are explained for those who are new in these fields of study.