spacecraft attitude determination and control pdf

Spacecraft attitude determination and control pdf

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Fundamentals of Spacecraft Attitude Determination and Control

Attitude control is the process of controlling the orientation of an aerospace vehicle with respect to an inertial frame of reference or another entity such as the celestial sphere , certain fields, and nearby objects, etc. Controlling vehicle attitude requires sensors to measure vehicle orientation, actuators to apply the torques needed to orient the vehicle to a desired attitude, and algorithms to command the actuators based on 1 sensor measurements of the current attitude and 2 specification of a desired attitude. The integrated field that studies the combination of sensors, actuators and algorithms is called guidance, navigation and control GNC.

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Skip to search form Skip to main content You are currently offline. Some features of the site may not work correctly. Save to Library. Create Alert. Launch Research Feed. Share This Paper. Figures and Tables from this paper. Figures and Tables. One Citation. Citation Type. Has PDF. Publication Type. More Filters. View 1 excerpt, cites methods.

Research Feed. Highly Influential. View 3 excerpts, references background and methods. Fundamentals of Spacecraft Attitude Determination and Control. View 9 excerpts, references background and methods. Spacecraft attitude determination and control: Quaternion based method. View 1 excerpt, references methods. Survey of nonlinear attitude estimation methods. View 2 excerpts, references background. Analytical Mechanics of Space Systems.

View 3 excerpts, references methods and background. Introduction to random signals and applied kalman filtering 3rd ed. View 7 excerpts, references background and methods.

Kalman filtering implementation with Matlab. View 1 excerpt, references background. How a Kalman filter works, in pictures. Related Papers. By clicking accept or continuing to use the site, you agree to the terms outlined in our Privacy Policy , Terms of Service , and Dataset License.

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Spacecraft pointing accuracies with sub-arcsec to milli-arcsec levels are becoming a norm for the future space missions, which is mainly achieved by employing mission-specific fine guidance sensor FGS. Furthermore, performance comparison between the rate-integrating and rate-gyroscope-based multiplicative extended Kalman filter for this mission is demonstrated. Finally, performance comparison of three attitude controllers establishes their feasibility for this mission. Google Scholar. G Google Scholar. Thesis, Massachusetts Inst.

F] Fundamentals of Spacecraft Attitude Determination and Control Read Online Details Details Product: This book explores topics that are central to the field of spacecraft attitude determination and control. The authors provide rigorous theoretical derivations of significant algorithms accompanied by a generous amount of qualitative discussions of the subject matter. The book documents the development of the important concepts and methods in a manner accessible to practicing engineers, graduate-level engineering students and applied mathematicians. It includes detailed examples from actual mission designs to help ease the transition from theory to practice and also provides prototype algorithms that are readily available on the author's website. Subject matter includes both theoretical derivations and practical implementation of spacecraft attitude determination and control systems. It provides detailed derivations for attitude kinematics and dynamics and provides detailed description of the most widely used attitude parameterization, the quaternion.


Roger D. Werking Head, Attitude Determination and Control Section National Attitude Hardware and Data Acquisition. Front Matter. Pages PDF.


Fundamentals of Spacecraft Attitude Determination and Control

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Attitude Determination and Control System design of KufaSat

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