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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Foundations of Space Dynamics - изображение 229

and consists of the acceleration towards the instantaneous centre of rotation, картинка 230, as well as that away from the instantaneous centre, картинка 231. Of the acceleration normal to the instantaneous radius vector Foundations of Space Dynamics - изображение 232, the term Foundations of Space Dynamics - изображение 233is caused by a change of the radius in the rotating coordinate frame, Foundations of Space Dynamics - изображение 234, whereas the other term, картинка 235, is due to the variation of the angular velocity of rotation, картинка 236, in the same rotating frame.

An alternative representation of the motion of the point P is via Cartesian coordinates , картинка 237, measured in a reference frame whose axes are fixed in space. Let us consider картинка 238as such a fixed, right‐handed coordinate system with картинка 239, and Foundations of Space Dynamics - изображение 240being the constant plane of rotation. The radius vector and its time derivatives in the fixed frame are then given by

(2.14) Foundations of Space Dynamics - изображение 241

(2.15) Foundations of Space Dynamics - изображение 242

(2.16) Foundations of Space Dynamics - изображение 243

In general, a time variation of the radius vector, картинка 244, gives rise to a radial acceleration, картинка 245, which is resolved in a fixed coordinate frame, картинка 246, without resorting to any rotational acceleration terms. Such a coordinate frame whose axes are fixed in space is termed an inertial reference frame , and the acceleration measured by such a frame is termed the inertial (or “true”) acceleration. The inertial acceleration, картинка 247, can be thought of as being directed towards (or away from) an instantaneous centre of rotation, which itself could be a moving point. For example, a point moving along an arc of a constant radius, Foundations of Space Dynamics - изображение 248, at a constant angular rate, картинка 249, has its acceleration directed towards the arc's centre, картинка 250.

2.3 Newton's Laws

In 1687 Newton gave his three famous laws of motion, which are valid for the motion of all objects (unless they are moving at speeds comparable to the speed of light). Stated briefly, they are the following:

1 An object continues to move in a straight line at a constant velocity, unless acted upon by a force applied to it by another object.

2 The time rate of change of the velocity (called the acceleration) of an object is directly proportional to the force applied to the object. The constant of proportionality is a property of the object, called the mass.

3 If an object, A, applies a force on another object, B, then B applies a force on A of the same magnitude, but opposite in direction to that applied by A.

The consequences of these laws are profound, as they govern the motion of all objects (which are moving quite slowly when compared to the speed of light 2). The first law implies that there is no absolute position in space, because two observers moving in parallel straight lines at a constant speed, картинка 251, relative to one another find two events separated in time to take place at different positions. Such observers can be regarded to be located at the origins of two different reference frames , картинка 252and картинка 253, such that the relative motion takes place along the parallel axes, картинка 254, and картинка 255. The distances travelled by a moving object during the time, Foundations of Space Dynamics - изображение 256, measured in the two frames are different, as given by the following Galilean transformation :

(2.17) Foundations of Space Dynamics - изображение 257

Newton's laws applied to a moving object are equally valid in the two reference frames, картинка 258and картинка 259; hence they are both referred to as inertial reference frames . Another consequence of the first law is that it postulates an absolute quantity called the time , which is the same in all reference frames, and is therefore unaffected by the motion. The second law assigns a property called the mass to all material objects, which can be determined by measuring the force applied to the object and the corresponding acceleration experienced by it, while the third law defines the force applied by two isolated objects upon each other.

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