1 |
Huang, C. Y., and Stengel, R. F., "Restructurable Control Using Proportional -Integral Implicit Model - Following," J. of Guidance, Control, and Dynamics, Vol. 13, No. 2, 1990, pp. 303-309.
DOI
|
2 |
Ochi, Y., "Application of Feedback Linearization Method in a Digitally Restructurable Flight Control System," J. of Guidance, Control, and Dynamics, Vol. 16, No. 1, 1993.
|
3 |
박창수, 허종, 탁민제, "진화알고리듬을 이용한 항공기 제어기 설계," 한국항공우주학회지 제27권 제4호, 1999, pp. 104-114.
|
4 |
송용규, 고이옥, "신경망 기법을 이용한 비선형 STT 미사일 자동조종장치의 구현," 한국항공우주학회지 제25권 제6호, 1997, pp. 134-141.
|
5 |
Napolitano, M. R., An, Y., and Seanor, B. A., "A fault tolerant flight control system for sensor and actuator failures using neural networks," Aircraft Design, Volume 3, Issue 2, June 2000, Pergamon, pp. 103-128.
DOI
ScienceOn
|
6 |
남윤수, 이은용, "항공기 구동장치 시스템의 고장감지기법," 한국항공우주학회지 제24권 제2호, 1996, pp. 106-115.
|
7 |
Song, Y., Campa, G., Napolitano, M. R., Seanor, B., and Perhinschi, M. G., "Online Parameter Estimation Techniques Comparison Within a Fault Tolerant Flight Control System, J. of Guidance, Control, and Dynamics, Vol. 25, No. 3, 2002, pp. 528-537.
DOI
ScienceOn
|
8 |
C. L. Chen and R. S. Nutter, "An Extended Back-Propagation Learning Algorithm by Using Heterogeneous Processing Units," Proc. of International Joint Conference on Neural Network (IJCNN '92), Baltimore, MD, June 1992.
|
9 |
Morse, W., and Ossman, K., "Flight Control Reconfiguration Using Model Reference Adaptive Control," Proc. 1988 ACC, June 1988, pp. 2219-2224.
|
10 |
Rattan, K. S., "Evaluation of Control Mixer Concept for Reconfiguration of Flight Control System," Proc. 22nd IEEE CDC, Piscataway, NJ, 1985, pp. 560-569.
|
11 |
Raja, S. J., and Silverthorn, J.T., "Use of the Pseudo-Inverse for Design of a Reconfigurable Flight Control System," AIAA Paper 85-1900, Aug. 1985.
|
12 |
Maybeck, P. S., and Pogoda, D. L., "Multiple Model Adaptive Controller for the STOL/F-15 with Sensor Actuator Failures," Proc. 28th IEEE CDC, Tampa, FL, Dec. 1989, pp. 1566-1572.
|
13 |
Maybeck, P. S., and Stevens, R. D., "Reconfigurable Flight Control Via Multiple Model Adaptive Control Methods," Proc. 29th IEEE CDC, Honolulu, HI, 1990, pp. 3351-3356.
|
14 |
Horowitz, I., Arnold, P.B., and Houpis, C. H., "YF-16 CCV Flight Control System Reconfiguration Design Using Quantitative Feedback Theory," Proc. National Aerospace and Electronics Conference, IEEE, New York, 1985.
|
15 |
J. Roskam, Airplane Flight Dynamics and Automatic Flight Controls: Part I., DARcorporation, Lawrence, Kansas, 1998.
|