"This volume considers the modern tactical missile, which has become a highly integrated package made up of many electronic, mechanical, electromechanical and pyrotechnic sub-systems. In addition to hardware, it also covers the guidance algorithm and workings of the missile autopilot. It demonstrates how all of the elements are integrated to function together in high-performance mode while maintaining cost effectiveness. This text offers unique coverage of the three major missile control components: guidance, control, and estimation. It includes contributed chapters from leading experts from six nations. Nonlinear control techniques and implementation issues are covered in detail"--
Advances in missile guidance, control, and estimation
2013
XXXVII, 682 S.
24 cm
Ill., graph. Darst.
Includes bibliographical references and index
Editors: S.N. Balakrishnan (Department of Mechanical and Aerospace Engineering, Missouri University of Science and Technology, Rolla, Missouri); A. Tsourdos (School of Engineering, Cranfield University, Swindon, UK); B.A. White (School of Engineering, Cranfield University, Swindon, UK)
Buch
Englisch
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