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"Spacecraft Attitude Control: A Linear Matrix Inequality Approach solves problems for spacecraft attitude control systems using convex optimization and, specifically, through a linear matrix inequality (LMI) approach. High-precision pointing and improved robustness in the face of external disturbances and other uncertainties are requirements for the current generation of spacecraft. This book presents an LMI approach to spacecraft attitude control and shows that all uncertainties in the maneuvering process can be solved numerically. It explains how a model-like state space can be developed through a mathematical presentation of attitude control systems, allowing the controller in question to be applied universally."--

Space vehicles --- Attitude control systems. --- Attitude control systems --- Mathematical models.

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Artificial satellites --- Attitude control systems.

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Space vehicles --- Attitude control systems. --- Attitude control systems (Astronautics) --- Control systems --- Actuators. --- Automatic control

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ADCS - Spacecraft Attitude Determination and Control provides a complete introduction to spacecraft control. The book covers all elements of attitude control system design, including kinematics, dynamics, orbits, disturbances, actuators, sensors, and mission operations. Essential hardware details are provided for star cameras, reaction wheels, sun sensors, and other key components. The book explores how to design a control system for a spacecraft, control theory, and actuator and sensor details. Examples are drawn from the author's 40 years of industrial experience with spacecraft such as GGS, GPS IIR, Mars Observer, and commercial communications satellites, and includes historical background and real-life examples.

Space vehicles --- Guidance systems (Flight) --- Attitude control systems (Astronautics) --- Attitude control systems. --- Guidance systems. --- Control systems

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Guided missiles --- Electronics in navigation. --- Magnetometers --- Attitude control systems.