Modeling and Control - Flexible Structure Spacecraft

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Installation dynamics, optimal thruster propulsion, and specific impulse thrust for reignitable fuel motors to regulate pointing error is obtained for geosynchronous (e.g., the Indian National Satellite, INSAT

Harcharan S. Kang

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Indian National Satellite | INFORMATICALT 2002 | Optimal Thruster Propulsion | Satellite |

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Added	22 Dec 2010
Updated	22 Dec 2010
Type	Journal
Year	2002
Where	INFORMATICALT
Authors	Harcharan S. Kang

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Modeling and Control - Flexible Structure Spacecraft

Indian National Satellite | INFORMATICALT 2002 | Optimal Thruster Propulsion | Satellite |

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