The book introduces the Embedded Model Control methodology for the design and implementation of attitude and orbit control systems. The logic architecture is organized around the embedded model of the spacecraft
Control moment gyroDual spinEnergy sink analysisGyroscopic attitude controlMajor-axis spinnerMomentum wheelNutation damperOblate vs. prolateThis chapter applies the equations of rigid body motion to the study of attitude dynamics of spacecraft. We begin with spin-stabilized spacecraft and find that only...
SPACECRAFT ATTITUDE DYNAMICS AND CONTROL by Vladimir A. Chobotov Orig. Ed. 1991, Reprint Ed. 2008 161 pp. ISBN 978-0-89464-069-8 $98.75 Presented here are the basic concepts, methods, and mathematical develop- ments which are necessary to understand spacecraft attitude dynamics and control....
天文导航、卫星姿态控制-overview of spacecraft of Attitude_Determination_Control Simulations of Relative Multiple Spacecraft Dynamics and Control with MATLAB-Simulink and Satelli Finite-time control for nonlinear spacecraft attitude based on terminal sliding mode technique Distributed attitude consensus of spac...
Roger D. Werking Head, Attitude Determination and Control Section National Aeronautics and Space Administration/ Goddard Space Flight Center Extensiye work has been done for many years in the areas of attitude determination, attitude prediction, and attitude control. During this time, it has been di...
This capstone course is the 3rd and final course of the specialization Advanced Spacecraft Dynamics and Control. It assumes you have completed the prior courses on "Attitude Control with Momentum Exchange Devices" and "Analytical Mechanics for Spacecraft Dynamics". This project course investigates the...
Modelling and simulation of spacecraft dynamics play a central role in the development process for spacecraft control systems. In particular, while the requirements for attitude and orbit control systems are becoming more and more stringent, there is also a need for adequate design tools in order ...
control methodology for the design and implementation of attitude and orbit control systems. the logic architecture is organized around the embedded model of the spacecraft and its surrounding environment. the model is compelled to include disturbance dynamics as a repository of the uncertainty that ...
and solving real-world engineering problems. For example, the author discusses orbital and rotational dynamics of spacecraft under a variety of environmental conditions, along with the realistic constraints imposed by available hardware. Among the topics covered are orbital dynamics, attitude dynamics, ...
Thomson W H 1963Introduction to space dynamics (New York: John Wiley) Google Scholar Wertz J R 1978Spacecraft attitude determination and control (Dordrecht: Reidel) Google Scholar Wilsky A S 1976Automatica 12: 601–611 Article Google Scholar Wilsky A S 1980IEEE Trans. Autom. Control AC-...