| 1 |
H.-Y. Ko, J.-H. Baek, and H.-S. Choi, "Autonomous Flight System of UAV through Global and Local Path Generation," Journal of Aerospace System Engineering, vol. 13, no. 3, pp. 15-22, Jun. 2019./
|
|
| 2 |
D. H. Kim and S. W. Kim, "Evaluation of structural safety of linear actuator for flap control of aircraft," Journal of Aerospace System Engineering, vol. 13, no. 4, pp. 66-73, Aug. 2019./
|
|
| 3 |
K. M. Back, H. B. Park, "A study on structural design and analysis of small engine test equipment for use in aircraft," Journal of Aerospace System Engineering, vol. 12, no. 1, pp. 42-46, 2018./
|
|
| 4 |
J. M. Tak, L. Q. Viet, and J. H. Hwang, "Hybrid Control of Aircraft Landing Gear using Magnetorheological Damper" Journal of Aerospace System Engineering, vol. 12, no. 1, pp. 1-9, February 2018./
|
|
| 5 |
Jung-hoon Lee and Joon-tae Kim, "A Study on the Design and Analysis of the Fuel Boost Pump Motor Assembly for the Aircraft," Journal of Aerospace System Engineering, vol. 12, No. 3, pp. 1-8, June 2018./
|
|
| 6 |
J. H. Shin, S. H. Jeong, G. H. Kang, H. S. Lee "A Study on the Improvement of Crack Propagation in Wing Root Fairing Support by Pre-load in Military Aircraft Production Process", Journal of Aerospace System Engineering, Vol.12, No.3, pp.38-44, June, 2018/
|
|
| 7 |
Park, H., "Study on Design, Manufacturing and Test Evaluation using Composite Materials of Vertical Axis Wind Turbine Blade," Journal of Aerospace System Engineering, Vol. 12, No. 3, pp. 58-63, 2018./
|
|
| 8 |
J. M. Tak et al., "Hybrid control of aircraft landing gear using magnetorheological", Journal of Aerospace System Engineering, vol. 12, no. 1, pp. 1-9, 2018./
|
|
| 9 |
K. Lee, K. Oh, "A Study on the Derivation of ConOps Sea-based Guided Weapon Systems" Journal of Aerospace System Engineering, Vol.11, No.5, pp.50-55, October, 2017/
|
|
| 10 |
J. Hur, K. Oh, "An Analysis of Weapon Systems Operational Requirements Document in National Defense Acquisition Process" Journal of Aerospace System Engineering, Vol.11, No.2, pp.1-8, April, 2017/
|
|