Ashish Tewari - Foundations of Space Dynamics

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Foundations of Space Dynamics offers an authoritative text that combines a comprehensive review of both orbital mechanics and dynamics. The author—a noted expert on the topic—covers up-to-date topics including: orbital perturbations, Lambert's transfer, formation flying, and gravity-gradient stabilization. The text provides an introduction to space dynamics in its entirety, including important analytical derivations and practical space flight examples. Written in an accessible and concise style, Foundations of Space Dynamics highlights analytical development and rigor, rather than numerical solutions via ready-made computer codes. To enhance learning, the book is filled with helpful tables, figures, exercises, and solved examples. This important book: Covers space dynamics with a systematic and comprehensive approach Designed to be a practical text filled with real-world examples Contains information on the most current applications Includes up-to-date topics from orbital perturbations to gravity-gradient stabilization Offers a deep understanding of space dynamics often lacking in other textbooks Written for undergraduate and graduate students and professionals in aerospace engineering, Foundations of Space Dynamics offers an introduction to the most current information on orbital mechanics and dynamics.

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(2.54) This implies that the particle motion takes place in a constant or invariant - фото 398

This implies that the картинка 399‐particle motion takes place in a constant (or invariant ) plane containing the centre of mass. The constant vector картинка 400is normal to the invariant plane, and is termed the net angular momentum of the system about the origin картинка 401. This is the law of conservation of angular momentum in the absence of a net external torque about картинка 402.

The conservation of linear and angular momentum, as well as the total energy of the картинка 403‐particle system, is valid for any system ruled only by gravitational forces. The conservation principles are also valid for картинка 404‐bodies of arbitrary shapes, as no restrictions have been applied in deriving those principles for the картинка 405‐particle system. A body is defined to be a collection of a large number of particles. Thus the particles can be grouped into several bodies, each translating and rotating with respect to a common reference frame. However, solving for the motion variables (linear and angular positions and velocities) of a system of картинка 406bodies (referred to as the картинка 407body problem ) requires a numerical determination of the individual gravity fields of the bodies, as well as an integration of the картинка 408first‐order, ordinary differential equations governing their motion. The next section discusses how such differential equations are derived for a body. The solar system is an example of the картинка 409‐body system. Numerical approximations and simplifying assumptions are invariably employed in the solution of the картинка 410‐body problem. For example, when the separations between the centres of mass of the respective bodies given by картинка 411, картинка 412, are always large, the problem is approximated as that of картинка 413‐bodies of spherical shape with radially symmetrical mass distributions.

2.6 Dynamics of a Body

The motion of a body is described by the motion of the particles constituting the body. A pure translation of a body is a motion in which all the particles constituting the body are moving in parallel straight lines with the same velocity. If the body is rigid, then the distance between any two of its particles is fixed; hence it is possible for the body to have a pure rotation , defined as the motion in which all the particles describe concentric circles about a fixed axis, and thus have velocities that are proportional to their respective distances from the axis of rotation. A rigid body in a combined translation and rotation has its constituent particles travelling in curved paths of different shapes relative to a stationary reference frame. A non‐rigid body can have structural deformation as it translates and rotates, wherein the relative distances of the particles varies with time. The general motion of a body therefore consists of a combination of translation, rotation, and structural deformation, whose complete description requires a determination of the spatial trajectories of the particles constituting the body.

Consider a body with the centre of mass, o , with a particle of elemental mass, d картинка 414, located at картинка 415relative to o (see Fig. 2.3). Also consider an inertial reference frame, OXYZ , with origin at картинка 416, and unit vectors, картинка 417, along картинка 418, картинка 419, and картинка 420, respectively. The positions of o and the elemental mass relative to the origin, картинка 421, are given by картинка 422and картинка 423, respectively, whose time derivatives in the inertial frame are the respective velocities, картинка 424and картинка 425. If the net force experienced by the elemental mass is d Foundations of Space Dynamics - изображение 426, then its equation of motion by Newton's second law is expressed as follows:

(2.55) Foundations of Space Dynamics - изображение 427

where the net force, d картинка 428, is a sum of all internal (d Foundations of Space Dynamics - изображение 429) and external (d Foundations of Space Dynamics - изображение 430) forces applied to the elemental mass, Foundations of Space Dynamics - изображение 431. The velocities, Foundations of Space Dynamics - изображение 432and Foundations of Space Dynamics - изображение 433, are related by the following kinematic equation:

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