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Chapter 1 - Introduction

Published online by Cambridge University Press:  18 December 2014

Marcel J. Sidi
Affiliation:
Israel Aircraft Industries Ltd
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Summary

Overview

Space technology is relatively young compared to other modern technologies, such as aircraft technology. However, in only forty years this novel domain has achieved a tremendous level of complexity and sophistication. The reason for this is simply explained: most satellites, once in space, must rely heavily on the quality of their onboard instrumentation and on the design ingenuity of the scientists and engineers who produced them. Recent achievements of repairing satellites while in orbit testify to the complexity involved in space technology. The desire of humans to conquer space within the solar system will surely encourage new technological achievements that are not yet imagined.

The technical fields in which satellites are used are numerous – telecommunications, scientific research, meteorology, and others. According to the specific task for which they are designed, satellites are very different from one another. They may be in orbits as low as 200 km or as high as 40,000 km above the earth; other spacecraft leave the earth toward planets in the solar system. Satellites may be very heavy: an inhabited space station, for example, could weigh several tons or more. There also exist very light satellites, weighing 20 kg or less. Small satellites may be relatively cheap, of the order of a million dollars apiece. Despite their differences, satellites possess fundamental features that are common to all. The physical laws that govern their motion in space and their dynamics are the same for all spacecraft. Hence, the fundamental technologies that evolved from these laws are common to all.

A satellite's life begins with the specific booster transferring it to some initial orbit, called a transfer orbit, in which the satellite is already circling the earth. For a satellite that will stay near earth, the next stage will be to “ameliorate” the orbit; this means that the satellite must be maneuvered to reach the precise orbit for which the satellite was designed to fulfill its mission. Next, the satellite's software must check for the proper functioning of its instrumentation and its performance in space, as well as calibrate some of the instruments before they can be used to control the satellite. The final stage is the one for which the satellite was designed and manufactured.

Type
Chapter
Information
Spacecraft Dynamics and Control
A Practical Engineering Approach
, pp. 1 - 7
Publisher: Cambridge University Press
Print publication year: 1997

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References

Bittner, H., Fisher, H., Miltenberger, K., Roche, Z. C., Scheit, A., Surauer, M., and Vieler, H. (1987), “The Attitude and Orbit Control Subsystem of the DFS Kopernikus,” Automatic Control World Congress, IFAC (27–31 July, Munich). Oxford: Pergamon.
Bittner, H., Fisher, H., Froeliger, J., Miltenberger, K., Popp, H., Porte, F., and Surauer, M. (1989), “The Attitude and Orbit Control Subsystem of the EUTELSAT II Spacecraft,” 11th IFAC Symposium on Automatic Control in Space (17–21 July, Tsukuba, Japan1).
Dougherty, H., Scott, E., and Rodden, J. (1968), “Analysis and Design of WHECON – An Attitude Control Concept,” Paper no. 68–461, AIAA 2nd Communications Satellite System Conference (8–10 April, San Francisco). New York: AIAA.

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  • Introduction
  • Marcel J. Sidi, Israel Aircraft Industries Ltd
  • Book: Spacecraft Dynamics and Control
  • Online publication: 18 December 2014
  • Chapter DOI: https://doi.org/10.1017/CBO9780511815652.002
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Save book to Dropbox

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  • Introduction
  • Marcel J. Sidi, Israel Aircraft Industries Ltd
  • Book: Spacecraft Dynamics and Control
  • Online publication: 18 December 2014
  • Chapter DOI: https://doi.org/10.1017/CBO9780511815652.002
Available formats
×

Save book to Google Drive

To save content items to your account, please confirm that you agree to abide by our usage policies. If this is the first time you use this feature, you will be asked to authorise Cambridge Core to connect with your account. Find out more about saving content to Google Drive.

  • Introduction
  • Marcel J. Sidi, Israel Aircraft Industries Ltd
  • Book: Spacecraft Dynamics and Control
  • Online publication: 18 December 2014
  • Chapter DOI: https://doi.org/10.1017/CBO9780511815652.002
Available formats
×