Research and Feasibility Study of Control Logic Techniques for Space Vehicle Attitude Controls

Research and Feasibility Study of Control Logic Techniques for Space Vehicle Attitude Controls PDF Author: L. R. Fenzel
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 238

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Research and Feasibility Study of Control Logic Techniques for Space Vehicle Attitude Controls

Research and Feasibility Study of Control Logic Techniques for Space Vehicle Attitude Controls PDF Author: L. R. Fenzel
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 238

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ASD Technical Report

ASD Technical Report PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 240

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U.S. Government Research Reports

U.S. Government Research Reports PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 216

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Technical Abstract Bulletin

Technical Abstract Bulletin PDF Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 824

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Commercial Satellite Launch Vehicle Attitude Control Systems Design and Analysis (H-infinity, Loop Shaping, and Coprime Approach)

Commercial Satellite Launch Vehicle Attitude Control Systems Design and Analysis (H-infinity, Loop Shaping, and Coprime Approach) PDF Author: Chong Hun Kim
Publisher: Lulu.com
ISBN: 0615165117
Category : Technology & Engineering
Languages : en
Pages : 676

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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.

Technical Publications Announcements with Indexes

Technical Publications Announcements with Indexes PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1556

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Feasibility Study of Optimum On-off Attitude Control System for Spacecraft

Feasibility Study of Optimum On-off Attitude Control System for Spacecraft PDF Author: John D. Regetz (Jr.)
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 36

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Feasibility study of high precision triaxial attitude control for spacecraft

Feasibility study of high precision triaxial attitude control for spacecraft PDF Author: General Electric Company. Spacecraft Dept
Publisher:
ISBN:
Category : Artificial satellites
Languages : en
Pages :

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Feasibility Study of Optimum On-off Attitude Control System for Spacecraft

Feasibility Study of Optimum On-off Attitude Control System for Spacecraft PDF Author: John D. Regetz
Publisher:
ISBN:
Category :
Languages : en
Pages : 23

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Technical Papers

Technical Papers PDF Author:
Publisher:
ISBN:
Category : Avionics
Languages : en
Pages : 456

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