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140122 ||| eng |
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|a 9781461510819
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100 |
1 |
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|a Wu, Keng C.
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245 |
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|a Transistor Circuits for Spacecraft Power System
|h Elektronische Ressource
|c by Keng C. Wu
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250 |
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|a 1st ed. 2003
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260 |
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|a New York, NY
|b Springer US
|c 2003, 2003
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300 |
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|a XIII, 218 p
|b online resource
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505 |
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|a I Part I -- 1 Junction Diode Circuits -- 2 Discrete Transistor Circuits -- 3 Operational Amplifiers -- 4 Transistors and Operational Amplifiers Combined- Medium Scale Circuit -- II Part II -- 5 Introduction of Spacecraft Power System -- 6 Boost Converter — Battery Discharger -- 7 Solar Array Shunt Regulators -- 8. Linear Shunt -- 9 Sequential Pulse Width Modulated Shunts -- 10 Free Running Switching Shunt --- Ripple Regulator -- 11 Switching-mode Battery Charger -- Reference
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653 |
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|a Automotive Engineering
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653 |
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|a Electrical and Electronic Engineering
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653 |
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|a Electrical engineering
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653 |
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|a Automotive engineering
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653 |
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|a Electronic circuits
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653 |
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|a Electronic Circuits and Systems
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041 |
0 |
7 |
|a eng
|2 ISO 639-2
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989 |
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|b SBA
|a Springer Book Archives -2004
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|a 10.1007/978-1-4615-1081-9
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|u https://doi.org/10.1007/978-1-4615-1081-9?nosfx=y
|x Verlag
|3 Volltext
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082 |
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|a 621.3815
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520 |
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|a As a stand-alone volume, Transistor Circuits For Spacecraft Power System presents numerous transistor circuits and building blocks associated with power electronics in general, and examines the major subsystem components for solar-based spacecraft power systems. The technique and concept, of "continuity of states" for nonlinear circuits handling power transfer under cyclic excitation is introduced in Part I and further developed throughout the book. This powerful technique employing matrix formulation bypasses eigen-transients and yields steady-state responses rapidly. Closed-loop treatments are also given for large-scale linear circuits, many closed-form solutions for control loop-gain, conducted susceptibility, output impedance, etc. are covered. Extensive mathematical procedures are retained to highlight the importance of analytical flows. The author also reviews the evolution of solar-based spacecraft power systems; introduces modes of operations: discharge (boost), shunt, and charge; and covers pulse-width-modulated (PWM) boost power converter for both DC and AC conditions. A configuration tree for shunt mode operation is conceived. Based on the configuration tree, the best topologies, sequential PWM shunt and ripple-regulated free-running shunt, are intensively examined and formulated. Transistor Circuits For Spacecraft Power System provides important information for understanding the relationship between earthbound semiconductor circuits and space borne vehicles
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