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Theoretical Basis of Launch Vehicle Ballistics and Control
This book explains in detail the basic principles of launch vehicle trajectory and ballistic design methods, and gradually guides readers to become familiar with guidance and attitude control technology. It focuses on theoretical knowledge such as perturbation guidance, explicit guidance, and combined guidance. On the basis of introducing the research methods for launch vehicle dynamic characteristics, it conducts an in-depth analysis of the longitudinal (lateral) dynamic characteristics of laun
76Reads8.6Score—Shelves
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This book first introduces the orbit and motion laws of artificial earth satellites. Based on an in-depth analysis of the two-body problem, through detailed theoretical derivation, the perturbation motion equation of satellite operation is established, and the first-order analytical solution of the perturbation motion equation is studied. Then, the application of satellite motion theory is systematically discussed. Using this method, we proposed solutions to the satellite orbit and launch sectio
45Reads5.8Score—Shelves