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| NO | Title, Author(s) (Publication Title, Volume Issue, Page, Issue Date) |
|---|---|
| A guidance law with a switching logic for maintaining seeker Sang, D.; Ryoo, C.-K.; Tahk, Min-Jea, AIAA Guidance, Navigation and Control Conference and Exhibit, 2008-08-18 | |
| Missile autopilot design via output redefinition and gain optimization technique Min, B.-M.; Sang, D.; Tahk, Min-Jea; Kim, B.-S., SICE(Society of Instrument and Control Engineers)Annual Conference, SICE 2007, pp.2615 - 2619, 2007-09-17 | |
| Direct trajectory optimization of a soft lunar landing considering a landing site Park, B.-G.; Sang, D.; Tahk, Min-Jea, 60th International Astronautical Congress 2009, IAC 2009, v.6, pp.4413 - 4423, 2009-10-12 | |
| Constrained trajectory optimization for lunar landing during the powered descent phase Park, B.-G.; Sang, D.; Tahk, Min-Jea, ICROS-SICE International Joint Conference 2009, ICCAS-SICE 2009, pp.4226 - 4231, 2009-08-18 | |
| Impact angle control guidance law using Lyapunov function and PSO method Sang, D.; Min, B.-M.; Tahk, Min-Jea, SICE(Society of Instrument and Control Engineers)Annual Conference, SICE 2007, pp.2253 - 2257, 123, 2007-09-17 |
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