Multi Stage Design Of An Optimal Momentum Management And Attitude Controller For The Space Station

The objective of this research is to use the H[subscript infinity] optimality criterion to design a controller for the linearized set of Space Station dynamics equations. Besides studying the various closed-loop properties of the resulting linear system, we would like to examine the robustness properties of this controller i.e. how well it performs in the presence of unmodelled dynamics, non-linearities and disturbances. Furthermore, we will compare and contrast the control action of the H[subscript infinity] controller with that of the LQR controller."

This book consists of one hundred and twenty-five selected papers presented at the 2015 International Conference on Applied Mechanics, Mechatronics and Intelligent Systems (AMMIS2015), which was held in Nanjing, China during June 19-20, 2015.AMMIS2015 focuses on seven main areas, namely, applied mechanics, control and automation, intelligent systems, computer technology, electronics engineering, electrical engineering, and materials science and technology. Experts in this field from all over the world contributed to the collection of research results and development activities.AMMIS2015 provides an excellent international exchange platform for researchers to share their development works and results in these areas. All papers selected for this proceeding were subjected to a rigorous peer-review process.

Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.