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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1.2.3 Synodic Frame

When two objects orbit one another at nearly constant rates on a fixed plane, a reference frame can be defined by two of its axes on the plane of rotation and rotating at the constant rate, and the third axis normal to the plane. Such a rotating reference frame is called a synodic frame . An example of a synodic frame is the ecliptic frame , which is a reference frame constructed out of the ecliptic plane, such as the frame картинка 109in Fig. 1.3. The motion of an object measured relative to a synodic frame must be corrected by a vector subtraction of the motion of the frame itself, as exemplified by the calculation of the sidereal day from the observed rotation in the ecliptic frame. The ecliptic frame has been used as a reference since the earliest days of astronomical observations. The division of the circle into картинка 110arose out of the apparent motion of the sun per day, which subtends an arc of one diameter every 12 hours when seen from Earth. Since the moon's apparent diameter from Earth is roughly the same as that of the sun, the eclipses of the sun and the moon are observed in the ecliptic (thus the name). However, since the moon's orbital plane around Earth is tilted картинка 111relative to the ecliptic, the eclipses happen only along the intersection (i.e., the line of nodes) of the two planes.

The Earth‐moon line provides another synodic reference frame for space flight. The Earth and the moon describe coplanar circles about the common centre of mass (called the barycentre ) every 27.32 mean solar days relative to the vernal equinox (called a sidereal month ). This rotational period appears in the synodic frame to be 29.53 mean solar days (a synodic month ) from one new moon to the next, which is obtained from the sidereal month by subtracting the rate of revolution of Earth‐moon system around the sun.

1.2.4 Julian Date

Instead of the calendar year of 365 mean solar days, the tropical year of 365.242 mean solar days, and the sidereal year of 365.25636 mean solar days, it is much more convenient to use a Julian year of 365.25 mean solar days, which avoids the addition of leap years in carrying out astronomical calculations. A Julian day number ( картинка 112) is defined to be the continuous count of the number of mean solar days elapsed since 12:00 noon universal time (UT) on January 1, 4713 BC. Universal time refers to the time taken as 12:00 noon when the sun is directly over the Greenwich meridian (which is defined to be zero longitude). The Julian day number 0 is assigned to the day starting at that time on the Julian proleptic calendar. The Julian date of a general time instant is expressed as the JDN plus the fraction of the 24‐hour day elapsed since the preceding noon UT. Julian dates are thus expressed as a Julian day number plus a decimal fraction. For example, the Julian date for 10:00 a.m. UT on April 21, 2020, is given by J2458960.91667, and the JDN is 2458960. Epochs are listed in ephemeris charts and nautical almanacs according to their Julian dates. Hence a Julian date serves as a common time measure for astronautical calculations involving two events separated in time.

Computation of the Julian date (JD) from a Gregorian calendar date is complicated due to the three calendar cycles used to produce the Julian calendar, namely the solar, the lunar, and the indiction cycles of 28, 19, and 15 year periods, respectively (Seidelmann, 1992). A product of these gives the Julian period of 7980 years. The Julian period begins from 4713 BC, which is chosen to be the first year of solar, lunar, and indiction cycles beginning together. The next epoch when the three cycles begin together will happen at noon UT on January 1, 3268. The following conversion formula for the JDN, truncated to the last integer, uses the numbering of the months from January to December as Foundations of Space Dynamics - изображение 113; the Gregorian calendar years are numbered such that the year 1 BC is the year zero, Foundations of Space Dynamics - изображение 114, (i.e., 2 BC is Foundations of Space Dynamics - изображение 115, 4713 BC is Foundations of Space Dynamics - изображение 116, etc.); and the day number, is the last completed day of the month up to noon UT 14 This formula - фото 117, is the last completed day of the month up to noon UT:

(1.4) This formula calculates the JDN for 0925 am UT on June 25 1975 by taking - фото 118

This formula calculates the JDN for 09:25 a.m. UT on June 25, 1975, by taking картинка 119, Foundations of Space Dynamics - изображение 120, Foundations of Space Dynamics - изображение 121, and yields the last truncated integer value as Foundations of Space Dynamics - изображение 122. Then the time elapsed from noon UT on June 24 to 09:25 a.m. UT on June 25 is added as a fraction to give the following Julian date:

An epoch in the Julian date is designated with the prefix and the suffix - фото 123

An epoch in the Julian date is designated with the prefix картинка 124, and the suffix being the closest Gregorian calendar date. For example, картинка 125refers to 12:00 noon UT on January 1, 2000, and has the Julian date of 2451545. Similarly, the epoch картинка 126, which occurs exactly 100 Julian years before 12:00 noon UT on January 1, 2000, must refer to 12 noon UT on January 0, 1900; hence its date in the Gregorian calendar is December 31, 1899, and its Julian date is 2415020. The difference in the epochs and is therefore mean solar days which is exactly 100 Julian years S - фото 127and is therefore mean solar days which is exactly 100 Julian years Since Julian - фото 128is therefore mean solar days which is exactly 100 Julian years Since Julian day numbers - фото 129mean solar days (which is exactly 100 Julian years).

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