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[1] Abramowitz, M., and Stegun, I., Handbook of Mathematical Functions, Dover Pub￾lications, New York, 1965. [2] Adair, R., Concepts in Physics, Academic Press, New York, 1969. [3] Anderson, J., and Ryon, J., Electromagnetic Radiation in Accelerated Systems, Physical Review, vol. 181, no. 5, pp. 1765–1775, May 1969
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Overview Ground Systems Support the space segment Command and Control Monitor spacecraft health Track Calculate spacecraft attitude
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Outline Definitions Software design process Design rules Software costing
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Space Systems Laboratory Massachusetts Institute of Technology Introduction Introduction Objective : To compare the different imaging configurations for a To compare the different imaging configurations for a Separated Spacecraft Interferometer operating from an Separated Spacecraft Interferometer operating from an Earth’s orbit Earth’s orbit
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— In order to point and slew optical systems, spacecraft attitude control provides coarse pointing while optics control provides fine pointing
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Space Systems Laboratory Massachusetts Institute of Technology Objective and Outline Objective and Outline Objective : To determine the optimal trajectories to re￾orient a cluster of spacecraft Motivation : To maximize the full potential of a cluster of spacecraft with minimal resources
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Overview Lecture Space Systems Engineering presented by: Prof. David Miller prepared by: Olivier de Weck Revised and augmented by: Soon-Jo Chung
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Electrical Power System Power Source Energy Storage Power Distribution Power Regulation and Control
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Systems Considerations (Valving, tanks, etc) Characteristics of some monopropellants (Reprinted from H. Koelle, Handbook of Astronautical Engineering, McGraw-Hill, 1961.) Flame Chemical Density temp
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The Jerome C Hunsaker Visiting Professor of Aerospace Systems Department of Aeronautical and Astronautical Engineering, Massachusetts Institute of Technology BIOGRAPHY Dr. Leopold had led the Arizona-based licensing and technology transfer business for Motorola Corporate Technology when
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