• Proceedings of the Korean Society of Precision Engineering Conference
• /
• 2008.11a
• /
• pp.537-538
• /
• 2008

• Proceedings of the Korean Society of Precision Engineering Conference
• /
• 2007.11a
• /
• pp.227-228
• /
• 2007

• Journal of Astronomy and Space Sciences
• /
• v.13 no.1
• /
• pp.48-54
• /
• 1996

The generalized linear impulsive correction problem is applied to make a linear programming problem for optimizing trajectory of an orbiting spacecraft. Numerical application for the stationkeeping maneuver problem of geostationary satellite shows that this problem can efficiently find the optimal solution of the stationkeeping parameters, such as velocity changes, and the points of impulse by using the revised simplex method.

• Proceedings of the Korean Society of Tribologists and Lubrication Engineers Conference
• /
• 2002.10b
• /
• pp.209-209
• /
• 2002

• Journal of the Korean Mathematical Society
• /
• v.34 no.4
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• pp.895-909
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• 1997

We state the necessary conditions on optimizing the parameters which the damping differential operators contain in abstract linear damped second order evolution equation on the Gelfand five fold.

• Proceedings of the Korean Society of Precision Engineering Conference
• /
• 2013.05a
• /
• pp.449-450
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• 2013

• Proceedings of the Korean Society of Precision Engineering Conference
• /
• 2013.05a
• /
• pp.643-644
• /
• 2013

• Proceedings of the Materials Research Society of Korea Conference
• /
• 2003.11a
• /
• pp.242-242
• /
• 2003

• Proceedings of the Korean Society of Precision Engineering Conference
• /
• 2010.05a
• /
• pp.993-994
• /
• 2010

• 한국전산유체공학회:학술대회논문집
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• 2008.08a
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• pp.42.6-43
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• 2008