Analytical Mechanics of Space Systems, Volum 1American Institute of Aeronautics and Astronautics, 2003 - 716 pàgines This single source provides a comprehensive treatment of dynamics of aerospace systems starting with the basic fundamentals. Topics range from basic kinematics and dynamics to more advanced celestial mechanics. It guides you through the various derivations and proofs, but avoids cookbook formulas. Instead, the reader is made to understand the underlying principle of the involved equations and shown how to apply them to various dynamical systems. The book is divided into two parts. Part I covers analytical treatment of topics such as basic dynamic principles up to advanced energy concept. Special attention is paid to the use of rotating reference frames that often occur in aerospace systems. Part II covers basic celestial mechanics treating the 2-body problem, restricted 3-body problem, gravity field modelling, perturbation methods, spacecraft formation flying, and orbit transfers. |
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Analytical Mechanics of Space Systems Hanspeter Schaub,John L. Junkins Previsualització limitada - 2003 |
Analytical Mechanics of Space Systems Hanspeter Schaub,John L. Junkins Previsualització no disponible - 2009 |
Frases i termes més freqüents
acceleration angular momentum angular momentum vector angular velocity angular velocity vector Assume asymptotic stability asymptotically axis center of mass chief orbit constant constraint coordinate system d'Alembert's principle defined definite differential equations direction cosine matrix disk dynamical system Earth eccentricity equations of motion Euler angles Euler parameter Example expressed feedback control law feedback gain force gimbal gimbal angles given gravitational Hamiltonian illustrated inertia matrix inertial initial integral kinematic kinetic energy Lagrange Lagrange's equations linear Lyapunov function m₁ m₂ motion in Eq nonlinear Note orbit elements orbit radius partial derivative particle position vector problem r₁ r₂ reference frame relative orbit rigid body scalar semimajor axis shown in Fig singular solution spacecraft stability steering law Substituting Eq three-body tion torque torque vector trajectory transformation true anomaly two-body variation written zero δω ән