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441 |
Thermomechanical Behaviors of Shape Memory Alloy Thin Films and Their Application
Jin-Ho Roh and In Lee
International Journal of Aeronautical and Space Sicences, vol. 7, no. 1, pp.91-98, 2006 |
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442 |
Nonlinear Aeroelastic Analysis of a High-Aspect-Ratio Wing with Large Deflection Effects
Kyung-seok Kim, In-Gyu Lim, In Lee/Jae-Han Yoo
International Journal of Aeronautical and Space Sicences, vol. 7, no. 1, pp.99-105, 2006 |
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443 |
Active Vibration Control of Composite Shell Structure using Modal Sensor/Actuator System
Seung Jo Kim, Joon Seok Hwang and Jiwon Mok
International Journal of Aeronautical and Space Sicences, vol. 7, no. 1, pp.106-117, 2006 |
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444 |
Auto-Landing Guidance System Design for Smart UAV
Byoung-Mun Min, Hyo-Sang Shin, Min-Jea Tahk, Boo Min Kim and Byoung Soo Kim
International Journal of Aeronautical and Space Sicences, vol. 7, no. 1, pp.118-128, 2006 |
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445 |
Guidance Synthesis to Control Impact Angle and Time
Hyo-Sang Shin, Jin-Ik Lee and Min-Jea Tahk
International Journal of Aeronautical and Space Sicences, vol. 7, no. 1, pp.129-136, 2006 |
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446 |
Stability Augmentation of Helicopter Rotor Blades Using Passive Damping of Shape Memory Alloys
Chul Yong Yun, Dae Sung Kim and Seung Jo Kim
International Journal of Aeronautical and Space Sicences, vol. 7, no. 1, pp.137-147, 2006 |
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447 |
Study on Satellite Vibration Control using Adaptive Control Scheme
Seboung Oh, Choong-Seok Oh and Hyochoong Bang
International Journal of Aeronautical and Space Sicences, vol. 6, no. 2, pp.1-16, 2005 |
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448 |
Development of Attitude Constraints for Real-time Attitude Determination System using GPS carrier phase
Jae-Gyu Jang and Chang-don Kee
International Journal of Aeronautical and Space Sicences, vol. 6, no. 2, pp.17-22, 2005 |
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449 |
Sliding Mode Trim and Attitude Control of a 2-DOF Rigid-Rotor Helicopter Model
Heon-Sul Jeong, Se-Myong Chang/ Jin-Sung Park
International Journal of Aeronautical and Space Sicences, vol. 6, no. 2, pp.23-32, 2005 |
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450 |
Improvement of Lift Dump on a Fighter-Type Wing at Approach Condition
Soojung Hwang/Ilwoo Lee
International Journal of Aeronautical and Space Sicences, vol. 6, no. 2, pp.33-45, 2005 |
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