메뉴 건너뛰기




Volumn 30, Issue 5, 2007, Pages 1399-1413

Digital autoland control laws using quantitative feedback theory and direct digital design

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT LANDING; CONTROL EQUIPMENT; FEEDBACK CONTROL; MICROSENSORS; PROBLEM SOLVING; TWO TERM CONTROL SYSTEMS; UNMANNED AERIAL VEHICLES (UAV);

EID: 35348987020     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.27761     Document Type: Article
Times cited : (48)

References (27)
  • 3
    • 0033904228 scopus 로고    scopus 로고
    • Automatic Landing System Design Using Fuzzy Logic
    • Feb
    • Nho, K., and Agarwal, R. K., "Automatic Landing System Design Using Fuzzy Logic," Journal of Guidance, Control, and Dynamics, Vol. 23, No. 2, Feb. 2000, pp. 298-304.
    • (2000) Journal of Guidance, Control, and Dynamics , vol.23 , Issue.2 , pp. 298-304
    • Nho, K.1    Agarwal, R.K.2
  • 4
    • 0242583008 scopus 로고    scopus 로고
    • Intelligent Automatic Landing System Using Time Delay Neural Network Controller
    • Juang, J.-G., and Chang, W.-B., "Intelligent Automatic Landing System Using Time Delay Neural Network Controller," Applied Artificial Intelligence, Vol. 17, No. 7, 2003, pp. 563-581.
    • (2003) Applied Artificial Intelligence , vol.17 , Issue.7 , pp. 563-581
    • Juang, J.-G.1    Chang, W.-B.2
  • 6
    • 35349008599 scopus 로고    scopus 로고
    • A Glidepath Tracking Algorithm for Autolanding of a UAV
    • AIAA Paper 2005-6979
    • Kim, D., Choi, Y., and Suk, J., "A Glidepath Tracking Algorithm for Autolanding of a UAV," AIAA Paper 2005-6979, 2005.
    • (2005)
    • Kim, D.1    Choi, Y.2    Suk, J.3
  • 7
    • 85087604723 scopus 로고    scopus 로고
    • Advanced Flight Control Technologies for UAVs, 2nd AIAA Unmanned-Unlimited Systems, Technologies, and Operations, San Diego, CA
    • AIAA Paper 2003-6537
    • Attar, M., Wahnon, E., and Chaimovitz, D., "Advanced Flight Control Technologies for UAVs," 2nd AIAA Unmanned-Unlimited Systems, Technologies, and Operations, San Diego, CA, AIAA Paper 2003-6537, 2003.
    • (2003)
    • Attar, M.1    Wahnon, E.2    Chaimovitz, D.3
  • 9
    • 19644361854 scopus 로고    scopus 로고
    • Davidson, R. W., Flight Control Design and Test of the Joint Unmanned Combat Air System J-UCAS X-45A, 3rd UnmannedUnlimited Technical Conference, Workshop, and Exhibit, Chicago, IL, AIAA Paper 2004-6557, 2004.
    • Davidson, R. W., "Flight Control Design and Test of the Joint Unmanned Combat Air System J-UCAS X-45A," 3rd "UnmannedUnlimited" Technical Conference, Workshop, and Exhibit, Chicago, IL, AIAA Paper 2004-6557, 2004.
  • 10
    • 35348938272 scopus 로고    scopus 로고
    • X-47A Pegasus Flight and Mission Systems Design and Test, 2nd Unmanned-Unlimited Systems, Technologies, and Operations, San Diego, CA
    • AIAA Paper 2003-6628
    • Wood, D., "X-47A Pegasus Flight and Mission Systems Design and Test," 2nd Unmanned-Unlimited Systems, Technologies, and Operations, San Diego, CA, AIAA Paper 2003-6628, 2003.
    • (2003)
    • Wood, D.1
  • 13
    • 0025536598 scopus 로고
    • Application of Quantitative Feedback Theory (QFT) to Flight Control Problems
    • Inst, of Electrical and Electronics Engineers, New York
    • Horowitz, I., "Application of Quantitative Feedback Theory (QFT) to Flight Control Problems," Proceedings of the 29th IEEE Conference on Decision and Control, Vol. 5, Inst, of Electrical and Electronics Engineers, New York, 1990, pp. 2593-2598.
    • (1990) Proceedings of the 29th IEEE Conference on Decision and Control , vol.5 , pp. 2593-2598
    • Horowitz, I.1
  • 14
    • 0028322834 scopus 로고
    • Design of Robust Quantitative Feedback Theory Controllers for Pitch Attitude Hold Systems
    • Bossert, D. E., "Design of Robust Quantitative Feedback Theory Controllers for Pitch Attitude Hold Systems," Journal of Guidance, Control, and Dynamics, Vol. 17, No. 1, 1994, pp. 217-219.
    • (1994) Journal of Guidance, Control, and Dynamics , vol.17 , Issue.1 , pp. 217-219
    • Bossert, D.E.1
  • 15
    • 0032108198 scopus 로고    scopus 로고
    • Introduction to Quantitative Feedback Theory for Lateral Robust Flight Control Systems Design
    • July
    • Wu, S., Grimble, M., and Breslin, S., "Introduction to Quantitative Feedback Theory for Lateral Robust Flight Control Systems Design," Control Engineering Practice, Vol. 6, No. 7, July 1998, pp. 805-828.
    • (1998) Control Engineering Practice , vol.6 , Issue.7 , pp. 805-828
    • Wu, S.1    Grimble, M.2    Breslin, S.3
  • 16
    • 0028748197 scopus 로고
    • Development and First Successful Flight Test of a QFT Flight Control System
    • Inst, of Electrical and Electronics Engineers, New York
    • Sheldon, S. N., and Rasmussen, S. J., "Development and First Successful Flight Test of a QFT Flight Control System," Proceedings of the IEEE 1994 National Aerospace and Electronics Conference, Vol. 1, Inst, of Electrical and Electronics Engineers, New York, 1994, pp. 629-636.
    • (1994) Proceedings of the IEEE 1994 National Aerospace and Electronics Conference , vol.1 , pp. 629-636
    • Sheldon, S.N.1    Rasmussen, S.J.2
  • 17
    • 0030242490 scopus 로고    scopus 로고
    • Development and Flight Testing of Quantitative Feedback Theory Pitch Rate Stability Augmentation System
    • Jr, Sept.-Oct
    • Fontenrose, P. L. and C. E. H., Jr., "Development and Flight Testing of Quantitative Feedback Theory Pitch Rate Stability Augmentation System," Journal of Guidance, Control, and Dynamics, Vol. 19, No. 5, Sept.-Oct. 1996, pp. 1109-1115.
    • (1996) Journal of Guidance, Control, and Dynamics , vol.19 , Issue.5 , pp. 1109-1115
    • Fontenrose, P.L.1    H., C.E.2
  • 18
    • 0242621810 scopus 로고    scopus 로고
    • Federal Aviation Administration, FAA, Anon
    • Anon., "Instrument Flying Handbook," Federal Aviation Administration, FAA-H-9093-15, 2001.
    • (2001) Instrument Flying Handbook
  • 20
    • 0037348985 scopus 로고    scopus 로고
    • Observer/Kalman Filter Identification for Online System Identification of Aircraft
    • Mar.-Apr
    • Valasek, J., and Chen, W., "Observer/Kalman Filter Identification for Online System Identification of Aircraft," Journal of Guidance, Control, and Dynamics, Vol. 26, No. 2, Mar.-Apr. 2003, pp. 347-353.
    • (2003) Journal of Guidance, Control, and Dynamics , vol.26 , Issue.2 , pp. 347-353
    • Valasek, J.1    Chen, W.2
  • 23
    • 84888656154 scopus 로고    scopus 로고
    • Anon., Military Standard Flying Qualities of Piloted Aircraft, U.S. Dept. of Defense, Rept. MIL-STD-1797a, Mar. 1990.
    • Anon., "Military Standard Flying Qualities of Piloted Aircraft," U.S. Dept. of Defense, Rept. MIL-STD-1797a, Mar. 1990.
  • 26
    • 84888735072 scopus 로고    scopus 로고
    • Anon., Flight Control Systems - Design, Installation and Test of Piloted Aircraft, General Specification For, U.S. Dept. of Defense, Rept. MIL-STD-9490D, 1964.
    • Anon., "Flight Control Systems - Design, Installation and Test of Piloted Aircraft, General Specification For," U.S. Dept. of Defense, Rept. MIL-STD-9490D, 1964.
  • 27
    • 0023138823 scopus 로고
    • Linear-Quadratic-Gaussian With Loop-Transfer-Recovery Methodology for an Unmanned Aircraft
    • Jan
    • Ridgely, D. B., Banda, S.S., McQuade, T. E., and Lynch, P. J., "Linear-Quadratic-Gaussian With Loop-Transfer-Recovery Methodology for an Unmanned Aircraft," Journal of Guidance, Control, and Dynamics, Vol. 10, No. 1, Jan. 1987, pp. 82-89.
    • (1987) Journal of Guidance, Control, and Dynamics , vol.10 , Issue.1 , pp. 82-89
    • Ridgely, D.B.1    Banda, S.S.2    McQuade, T.E.3    Lynch, P.J.4


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.