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Results 1-10 of 169 (Search time: 0.005 seconds).

NO Title, Author(s) (Publication Title, Volume Issue, Page, Issue Date)
1
New Structure for an Aerodynamic Fin Control System for Tail Fin-Controlled STT Missiles

Kim, Seung-Hwan; Lee, Yong-In; Tahk, Min-Jea, JOURNAL OF AEROSPACE ENGINEERING, v.24, no.4, pp.505 - 510, 2011-10

2
Conceptual Design of a Multi-Rotor Unmanned Aerial Vehicle Based on an Axiomatic Design

Yoo, Dong-Wan; Won, Dae-Yeon; Tahk, Min-Jea, INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES , v.11, no.2, pp.126 - 130, 2010-06

3
Guidance law switching logic considering the seekers field-of-view limits

Sang, DaeKyu; Tahk, Min-Jea, PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, v.223, no.G8, pp.1049 - 1058, 2009-12

4
Trajectory Optimization for a Supersonic Air-Breathing Missile System Using Pseudo-Spectral Method

Park Jung-Woo; Tahk, Min-Jea; Sung Hong-Gye, INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, v.10, no.1, pp.112 - 121, 2009-05

5
Hessian approximation algorithms for hybrid optimization methods

Tahk, Min-Jea; Park, Moon-Su; Woo, Hyun-k; Kim, Hyoun-Jin, ENGINEERING OPTIMIZATION, v.41, no.7, pp.609 - 633, 2009-07

6
Roll-Pitch-Yaw Integrated Robust Autopilot Design for a High Angle-of-Attack Missile

Kang, Seonhyeok; Kim, H. Jin; Lee, Jin-Ik; Jun, Byung-Eul; Tahk, Min-Jea, JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, v.32, no.5, pp.1622 - 1628, 2009-09

7
Missile acceleration controller design using proportional-integral and non-linear dynamic control design method

Kim, Seung-Hwan; Tahk, Min-Jea, PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, v.226, no.G8, pp.882 - 897, 2012-08

8
Three-Dimensional Trajectory Optimization of Soft Lunar Landings from the Parking Orbit with Considerations of the Landing Site

Park, Bong-Gyun; Tahk, Min-Jea, INTERNATIONAL JOURNAL OF CONTROL AUTOMATION AND SYSTEMS, v.9, no.6, pp.1164 - 1172, 2011-12

9
Dynamic Modeling and Stabilization Techniques for Tri-Rotor Unmanned Aerial Vehicles

Yoo, Dong-Wan; Oh, Hyon-Dong; Won, Dae-Yeon; Tahk, Min-Jea, INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES , v.11, no.3, pp.167 - 174, 2010-09

10
Multi-model approaches to three-axis missile autopilot design under aerodynamic roll angle uncertainty

Won, Dae-Yeon; Tahk, Min-Jea; Kim, Y-H; Kim, H. J., PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, v.226, no.G9, pp.1061 - 1077, 2012-09

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