Showing results 3 to 7 of 7
Guidance law for automatic landing of tilt-rotor aircraft Min, B.-M.; Tahk, Min-Jea; Kim, B.-S.; Shin, H.-S., AIAA Guidance, Navigation, and Control Conference 2005, v.6, pp.4756 - 4767, 2005-08-15 |
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 |
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 |
Suboptimal guidance laws with terminal jerk constraint Lee, J.-I.; Min, B.-M.; Tahk, Min-Jea, International Conference on Control, Automation and Systems, ICCAS 2007, pp.1399 - 1403, 2007-10-17 |
Unmanned autonomous helicopter system design and its flight test Min, B.-M.; Lee, I.-H.; Bang, Hyochoong; Tahk, Min-Jea; Hwang, T.-W.; Hong, J.-S., International Conference on Control, Automation and Systems, ICCAS 2007, pp.2090 - 2095, 2007-10-17 |
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