The key idea of this book was to model a landing gear for the analysis of the behavior of an aircraft during ground maneuvers. The aircraft landing gear by its nature itself is a complex multi-degree-of-freedom system. Based on stability criterion a suitable landing gear was selected for RLV. In this book landing gear is modeled exclusively as two DOF and for getting the individual responses of components it is also modeled as four DOF system subjected to smooth landing and suitable ground excitation. This book also provides the systematic way of solving complex multi-degree-of-freedom...